import OAI.MathematicalPhysics.Boltzmann.Approximation.CapActualLossDensity import OAI.MathematicalPhysics.Boltzmann.Approximation.CapHotSourceIntegrability import OAI.MathematicalPhysics.Boltzmann.Approximation.CapHotTransportBalance import OAI.MathematicalPhysics.Boltzmann.Approximation.CapMixedCollisionLimits import OAI.MathematicalPhysics.Boltzmann.Approximation.CapNonlinearHotLimit import OAI.MathematicalPhysics.Boltzmann.Branching.CentralRetainedLimit import OAI.MathematicalPhysics.Boltzmann.Branching.CharacteristicPhysicalGain import OAI.MathematicalPhysics.Boltzmann.Branching.CharacteristicProductTest import OAI.MathematicalPhysics.Boltzmann.Branching.HotChartHomeomorph import OAI.MathematicalPhysics.Boltzmann.Branching.HotPositiveRegion import OAI.MathematicalPhysics.Boltzmann.Branching.IncomingLossRate import OAI.MathematicalPhysics.Boltzmann.Branching.MixedPhysicalMeasures import OAI.MathematicalPhysics.Boltzmann.Branching.ProjectedTimeBalance import OAI.MathematicalPhysics.Boltzmann.Branching.SeparatedMeasureTail import OAI.MathematicalPhysics.Boltzmann.Branching.VanishingCutoffCollision import OAI.MathematicalPhysics.Boltzmann.Collision.CollisionSources import OAI.MathematicalPhysics.Boltzmann.Jets.ColdCentralVanishing namespace OAI section /-! # The physical hot collision decomposition on each compact time cylinder -/ noncomputable section open MeasureTheory Filter Set open scoped Topology ENNReal open BoltzmannNonuniqueness.VelocityWeight BoltzmannNonuniqueness.CollisionCompactness namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q} theorem eventually_hot_collision_identity (hcarleman : Published.GPV2009CarlemanInput) (S : AttainedCapSequence F) (hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2) (hK : 0 ≤ K) (hd₀ : 0 ≤ d₀) (hq₁ : 1 < q) (hq₂ : q < 2) {κ : ℕ → ℕ} {U : ℝ≥0∞} (hU : Tendsto (fun n => S.normalizedHorizon (κ n)) atTop (𝓝 U)) {a A R : ℝ} (ha : 0 ≤ a) (hA : ENNReal.ofReal A < U) : ∀ᶠ n in atTop, ∀ᵐ z ∂(coldCylinderVolume a A R).prod volume, S.hotSourceDensity a A (κ n) z = 2*mixedGainDensity (F.indices (κ n)+1) (S.rescaledColdDensity (κ n)) (S.hotDensity (κ n)) z- S.hotDensity (κ n) z*KineticCollisionNullSets.frequency (F.indices (κ n)+1) (S.rescaledColdDensity (κ n)) z+ (S.radius (κ n))^2*collisionSource (F.indices (κ n)+1) (S.hotDensity (κ n)) z+ H q z.2*S.rescaledColdSource (κ n) (z.1.1,(z.1.2,z.2)) := by filter_upwards [S.eventually_extendedHot_eq hs₀ hU hA] with n hn have ht : ∀ᵐ z ∂(coldCylinderVolume a A R).prod (volume : Measure Velocity), z.1.1 ∈ Icc a A := Measure.quasiMeasurePreserving_fst.ae (Measure.quasiMeasurePreserving_fst.ae (ae_restrict_mem measurableSet_Icc)) have hg : ∀ᵐ z ∂(coldCylinderVolume a A R).prod (volume : Measure Velocity), z.2 ∈ HotRepresentative.good q := Measure.quasiMeasurePreserving_snd.ae (HotRepresentative.ae_good hcarleman hq₁ hq₂) filter_upwards [ht,hg] with z hz hzg have he (v : Velocity) : S.hotDensity (κ n) (z.1,v) = S.physicalHotDensity (κ n) (z.1,v) := hn z.1.1 ⟨ha.trans hz.1,hz.2⟩ (z.1.2,v) have hi := S.rescaled_hot_collision hs₀ hsmax hη hηmax hK hd₀ hq₂ (κ n) z hzg rw [mixedGain_fiber_congr _ (fun _ => rfl) (fun v => (he v).symm) z.2, collisionSource_fiber_congr _ (fun v => (he v).symm) z.2,← he z.2] at hi rw [hotSourceDensity,indicator_of_mem (show z ∈ {z : HotKineticPhase | z.1.1 ∈ Icc a A} from hz)] exact hi end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence end end section /-! # General compact kinetic tests for the actual loss measure limit -/ noncomputable section open MeasureTheory Set Filter open scoped ENNReal Topology BoundedContinuousFunction open BoltzmannNonuniqueness.CollisionCompactness namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q} {S : AttainedCapSequence F} theorem HotPairExtraction.loss_measure_compact_limit (hcarleman : Published.GPV2009CarlemanInput) (hGLPS : Published.GLPS1988Proposition3) (E : HotPairExtraction S) (hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2) (hK : 0 ≤ K) (hα : 0 < α) (hαmax : α ≤ 1/4) (hγ : 0 < γ) (hd₀ : 0 < d₀) (hd₀max : d₀ ≤ 1) (hsmall : JetComparisonCoefficient.coefficient K*d₀*s₀^9 ≤ 1) (hq₁ : 1 < q) (hq₂ : q < 2) {a A R : ℝ} (ha : 0 < a) (haA : a ≤ A) (hA : ENNReal.ofReal A < E.horizon) (hR : 0 ≤ R) (ψ : C(HotKineticPhase,ℝ)) (hc : HasCompactSupport ψ) : Tendsto (fun n => ∫ z, ψ z ∂S.physicalLossMeasure a A R (E.indices n)) atTop (𝓝 (∫ z, ψ z ∂incomingLossMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))) := by let ν := incomingLossMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)) let _ : IsFiniteMeasure ν := E.toHotLimitExtraction.incomingLossMeasure_finite ha (ha.le.trans haA) hK hα hγ hq₂ have hfin := (S.eventually_physicalCollisionMeasures_finite hs₀ hsmax hη hηmax hK hα (hαmax.trans (by norm_num)) hγ hd₀ hd₀max hsmall hq₂ E.indices_strict E.horizon_limit (R := R) ha haA hA).mono (fun _ hn => hn.2) have hsep (u : (ℝ × JetPrototype.Space) →ᵇ ℝ) (v : Velocity →ᵇ ℝ) : Tendsto (fun n => ∫ z, u z.1*v z.2 ∂S.physicalLossMeasure a A R (E.indices n)) atTop (𝓝 (∫ z, u z.1*v z.2 ∂ν)) := E.loss_measure_separated_limit hcarleman hGLPS hs₀ hsmax hη hηmax hK hα hαmax hγ hd₀ hd₀max hsmall hq₁ hq₂ ha haA hA hR u.continuous.measurable (fun x => u.norm_coe_le_norm x) v.continuous (fun x => v.norm_coe_le_norm x) obtain ⟨RX,hRX⟩ := (hc.isCompact.image continuous_fst).isBounded.subset_closedBall (0 : ℝ × JetPrototype.Space) obtain ⟨RV,hRV⟩ := (hc.isCompact.image continuous_snd).isBounded.subset_closedBall (0 : Velocity) apply SeparatedTests.compact_test_tendsto_of_eventually_finite _ ν hfin hsep ψ hc 0 0 RX RV intro z hz apply image_eq_zero_of_notMem_tsupport intro hzs exact hz ⟨hRX ⟨z,hzs,rfl⟩,hRV ⟨z,hzs,rfl⟩⟩ end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence end end section /-! # Source identity with exactly the physical error controlled by compactness -/ noncomputable section open MeasureTheory Filter Set open scoped Topology ENNReal open BoltzmannNonuniqueness.CollisionCompactness namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q} theorem eventually_hot_source_error_identity (hcarleman : Published.GPV2009CarlemanInput) (S : AttainedCapSequence F) (hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2) (hK : 0 ≤ K) (hd₀ : 0 ≤ d₀) (hq₁ : 1 < q) (hq₂ : q < 2) {κ : ℕ → ℕ} {U : ℝ≥0∞} (hU : Tendsto (fun n => S.normalizedHorizon (κ n)) atTop (𝓝 U)) {a A R : ℝ} (ha : 0 ≤ a) (hA : ENNReal.ofReal A < U) : ∀ᶠ n in atTop, ∀ᵐ z ∂(coldCylinderVolume a A R).prod volume, S.hotSourceDensity a A (κ n) z = 2*mixedGainDensity (F.indices (κ n)+1) (S.rescaledColdDensity (κ n)) (S.hotDensity (κ n)) z- S.hotDensity (κ n) z*KineticCollisionNullSets.frequency (F.indices (κ n)+1) (S.rescaledColdDensity (κ n)) z+S.physicalCollisionError a A (κ n) z := by filter_upwards [S.eventually_hot_collision_identity hcarleman hs₀ hsmax hη hηmax hK hd₀ hq₁ hq₂ hU (R := R) ha hA,S.eventually_extendedHot_eq hs₀ hU hA] with n hn hext have ht : ∀ᵐ z ∂(coldCylinderVolume a A R).prod (volume : Measure Velocity), z.1.1 ∈ Icc a A := Measure.quasiMeasurePreserving_fst.ae (Measure.quasiMeasurePreserving_fst.ae (ae_restrict_mem measurableSet_Icc)) filter_upwards [hn,ht] with z hz hzt have he (v : Velocity) : S.hotDensity (κ n) (z.1,v) = S.physicalHotDensity (κ n) (z.1,v) := hext z.1.1 ⟨ha.trans hzt.1,hzt.2⟩ (z.1.2,v) rw [collisionSource_fiber_congr _ he z.2] at hz unfold physicalCollisionError coldSourceDensity rw [indicator_of_mem (show z ∈ {z : HotKineticPhase | z.1.1 ∈ Icc a A} from hzt)] simpa only [add_assoc] using hz end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence end end section /-! # Identification of the actual rescaled hot source against separated tests -/ noncomputable section open MeasureTheory Filter open scoped Topology ENNReal open BoltzmannNonuniqueness.CollisionCompactness namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q} {S : AttainedCapSequence F} theorem HotPairExtraction.hot_source_weak_limit (hDP : Published.DunfordPettis1940HotPairWindows) (hcarleman : Published.GPV2009CarlemanInput) (hGLPS : Published.GLPS1988Proposition3) (E : HotPairExtraction S) (hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2) (hK : 0 ≤ K) (hα : 0 < α) (hαmax : α ≤ 1/4) (hγ : 0 < γ) (hd₀ : 0 < d₀) (hd₀max : d₀ ≤ 1) (hsmall : JetComparisonCoefficient.coefficient K*d₀*s₀^9 ≤ 1) (hq₁ : 1 < q) (hq₂ : q < 2) : ∃ κ : ℕ → ℕ, StrictMono κ ∧ ∀ a A R : ℝ, ∀ ha : 0 < a, a ≤ A → ENNReal.ofReal A < E.horizon → 0 ≤ R → ∀ (θ : ℝ × JetPrototype.Space → ℝ), Measurable θ → ∀ B : ℝ, (∀ x, |θ x| ≤ B) → ∀ (φ : Velocity → ℝ), Continuous φ → ∀ C : ℝ, (∀ v, |φ v| ≤ C) → Tendsto (fun n => ∫ z, (θ z.1*φ z.2)*S.hotSourceDensity a A (E.indices (κ n)) z ∂(coldCylinderVolume a A R).prod volume) atTop (𝓝 (2*(∫ z, θ z.1*incomingGainTest φ z.2 ∂E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))- (∫ z, θ z.1*incomingLossTest φ z.2 ∂E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))) := by obtain ⟨κ,hκ,herr⟩ := E.vanishing_physical_collision_error hDP hcarleman hGLPS hs₀ hsmax hη hηmax hK hα (hαmax.trans (by norm_num)) hγ hd₀ hd₀max hsmall hq₁ hq₂ refine ⟨κ,hκ,fun a A R ha haA hA hR θ hθ B hθB φ hφ C hφC => ?_⟩ let ψ : HotKineticPhase → ℝ := fun z => θ z.1*φ z.2 have hψ : Measurable ψ := (hθ.comp measurable_fst).mul (hφ.measurable.comp measurable_snd) have hB : 0 ≤ B := (abs_nonneg (θ (0,0))).trans (hθB _) have hC : 0 ≤ C := (abs_nonneg (φ 0)).trans (hφC _) have hψB (z) : |ψ z| ≤ B*C := by exact (abs_mul _ _).trans_le (mul_le_mul (hθB _) (hφC _) (abs_nonneg _) hB) have he := Compactness.bounded_test_integral_tendsto_zero (fun n => (S.physicalCollisionError_measurable hs₀ hsmax hη hηmax hK hd₀.le hq₂ a A (E.indices (κ n))).aestronglyMeasurable) (herr a A R ha haA hA) hψ (mul_nonneg hB hC) hψB have hg := (E.mixed_physical_gain_limit hcarleman hGLPS hs₀ hsmax hη hηmax hK hα hαmax hγ hd₀ hd₀max hsmall hq₁ hq₂ ha haA hA hR hθ hθB hφ hφC).comp hκ.tendsto_atTop have hl := (E.mixed_physical_loss_limit hcarleman hGLPS hs₀ hsmax hη hηmax hK hα hαmax hγ hd₀ hd₀max hsmall hq₁ hq₂ ha haA hA hR hθ hθB hφ hφC).comp hκ.tendsto_atTop have ht := ((hg.const_mul 2).sub hl).add he simp only [add_zero] at ht apply ht.congr' have hei : ∀ᶠ n in atTop, Integrable (S.physicalCollisionError a A (E.indices (κ n))) ((coldCylinderVolume a A R).prod volume) := ((herr a A R ha haA hA).eventually (eventually_lt_nhds (show (0 : ℝ≥0∞) < ⊤ from ENNReal.coe_lt_top))).mono (fun _ hn => memLp_one_iff_integrable.mp hn) filter_upwards [S.eventually_hot_source_error_identity hcarleman hs₀ hsmax hη hηmax hK hd₀.le hq₁ hq₂ (E.horizon_limit.comp hκ.tendsto_atTop) (R := R) ha.le hA, S.eventually_mixedPreRate_integrable hs₀ hsmax hη hηmax hK hα (hαmax.trans (by norm_num)) hγ hd₀ hd₀max hsmall hq₂ (E.indices_strict.comp hκ) (E.horizon_limit.comp hκ.tendsto_atTop) (R := R) ha haA hA,hei] with n hn hpre hei have hp := hpre (S.collisionCutoff (E.indices (κ n))) have hgi := mixed_gain_test_integrable hp hψ hψB have hli := mixed_loss_test_integrable hp hψ hψB have heψ := hei.bdd_mul hψ.aestronglyMeasurable (ae_of_all _ hψB) dsimp only [Function.comp_def,ψ] at hgi hli heψ ⊢ have hsum := integral_add ((hgi.const_mul 2).sub hli) heψ simp only [Pi.sub_apply] at hsum rw [← integral_const_mul,← integral_sub (hgi.const_mul 2) hli,← hsum] apply integral_congr_ae filter_upwards [hn] with z hz rw [hz] change _ = (θ z.1*φ z.2)*(2*mixedGainDensity (S.collisionCutoff (E.indices (κ n))) (S.rescaledColdDensity (E.indices (κ n))) (S.hotDensity (E.indices (κ n))) z- S.hotDensity (E.indices (κ n)) z*KineticCollisionNullSets.frequency (S.collisionCutoff (E.indices (κ n))) (S.rescaledColdDensity (E.indices (κ n))) z+ S.physicalCollisionError a A (E.indices (κ n)) z) ring end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence end end section /-! # Separated-test convergence of the actual physical gain measures -/ noncomputable section open MeasureTheory Set Filter open scoped ENNReal Topology open BoltzmannNonuniqueness.CollisionCompactness namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q} {S : AttainedCapSequence F} theorem HotPairExtraction.gain_measure_separated_limit (hcarleman : Published.GPV2009CarlemanInput) (hGLPS : Published.GLPS1988Proposition3) (E : HotPairExtraction S) (hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2) (hK : 0 ≤ K) (hα : 0 < α) (hαmax : α ≤ 1/4) (hγ : 0 < γ) (hd₀ : 0 < d₀) (hd₀max : d₀ ≤ 1) (hsmall : JetComparisonCoefficient.coefficient K*d₀*s₀^9 ≤ 1) (hq₁ : 1 < q) (hq₂ : q < 2) {a A R : ℝ} (ha : 0 < a) (haA : a ≤ A) (hA : ENNReal.ofReal A < E.horizon) (hR : 0 ≤ R) {B : ℝ} {θ : ℝ × JetPrototype.Space → ℝ} (hθ : Measurable θ) (hθB : ∀ x, |θ x| ≤ B) {φ : Velocity → ℝ} (hφ : Continuous φ) {C : ℝ} (hφC : ∀ v, |φ v| ≤ C) : Tendsto (fun n => ∫ z, θ z.1*φ z.2 ∂S.physicalGainMeasure a A R (E.indices n)) atTop (𝓝 (∫ z, θ z.1*φ z.2 ∂incomingGainMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))) := by let μ := E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R) let _ : SFinite μ := by dsimp [μ,HotLimitExtraction.mixedMeasure]; infer_instance have hi : Integrable incomingRate μ := E.toHotLimitExtraction.incomingRate_integrable ha (ha.le.trans haA) hK hα hγ hq₂ have hB : 0 ≤ B := (abs_nonneg (θ (0,0))).trans (hθB _) have ht := E.mixed_physical_gain_limit hcarleman hGLPS hs₀ hsmax hη hηmax hK hα hαmax hγ hd₀ hd₀max hsmall hq₁ hq₂ ha haA hA hR hθ hθB hφ hφC rw [← incomingGainMeasure_separated hi hθ hB hθB hφ.measurable hφC] at ht apply ht.congr' filter_upwards [S.eventually_mixedPreRate_integrable hs₀ hsmax hη hηmax hK hα (hαmax.trans (by norm_num)) hγ hd₀ hd₀max hsmall hq₂ E.indices_strict E.horizon_limit (R := R) ha haA hA] with n hn have hc := fun p => (S.rescaledColdDensity_bounds hs₀ hsmax hη hηmax hK hd₀.le hq₂ (E.indices n) p).1 have hh := S.hotDensity_nonneg hs₀ hsmax hη hηmax hK hd₀.le hq₂ (E.indices n) exact (mixedGainMeasure_integral hc hh (hn _) (fun z => θ z.1*φ z.2)).symm end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence end end section /-! # General compact kinetic tests for the actual gain measure limit -/ noncomputable section open MeasureTheory Set Filter open scoped ENNReal Topology BoundedContinuousFunction open BoltzmannNonuniqueness.CollisionCompactness namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q} {S : AttainedCapSequence F} theorem HotPairExtraction.gain_measure_compact_limit (hcarleman : Published.GPV2009CarlemanInput) (hGLPS : Published.GLPS1988Proposition3) (E : HotPairExtraction S) (hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2) (hK : 0 ≤ K) (hα : 0 < α) (hαmax : α ≤ 1/4) (hγ : 0 < γ) (hd₀ : 0 < d₀) (hd₀max : d₀ ≤ 1) (hsmall : JetComparisonCoefficient.coefficient K*d₀*s₀^9 ≤ 1) (hq₁ : 1 < q) (hq₂ : q < 2) {a A R : ℝ} (ha : 0 < a) (haA : a ≤ A) (hA : ENNReal.ofReal A < E.horizon) (hR : 0 ≤ R) (ψ : C(HotKineticPhase,ℝ)) (hc : HasCompactSupport ψ) : Tendsto (fun n => ∫ z, ψ z ∂S.physicalGainMeasure a A R (E.indices n)) atTop (𝓝 (∫ z, ψ z ∂incomingGainMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))) := by let ν := incomingGainMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)) let _ : IsFiniteMeasure ν := E.toHotLimitExtraction.incomingGainMeasure_finite ha (ha.le.trans haA) hK hα hγ hq₂ have hfin := (S.eventually_physicalCollisionMeasures_finite hs₀ hsmax hη hηmax hK hα (hαmax.trans (by norm_num)) hγ hd₀ hd₀max hsmall hq₂ E.indices_strict E.horizon_limit (R := R) ha haA hA).mono (fun _ hn => hn.1) have hsep (u : (ℝ × JetPrototype.Space) →ᵇ ℝ) (v : Velocity →ᵇ ℝ) : Tendsto (fun n => ∫ z, u z.1*v z.2 ∂S.physicalGainMeasure a A R (E.indices n)) atTop (𝓝 (∫ z, u z.1*v z.2 ∂ν)) := E.gain_measure_separated_limit hcarleman hGLPS hs₀ hsmax hη hηmax hK hα hαmax hγ hd₀ hd₀max hsmall hq₁ hq₂ ha haA hA hR u.continuous.measurable (fun x => u.norm_coe_le_norm x) v.continuous (fun x => v.norm_coe_le_norm x) obtain ⟨RX,hRX⟩ := (hc.isCompact.image continuous_fst).isBounded.subset_closedBall (0 : ℝ × JetPrototype.Space) obtain ⟨RV,hRV⟩ := (hc.isCompact.image continuous_snd).isBounded.subset_closedBall (0 : Velocity) apply SeparatedTests.compact_test_tendsto_of_eventually_finite _ ν hfin hsep ψ hc 0 0 RX RV intro z hz apply image_eq_zero_of_notMem_tsupport intro hzs exact hz ⟨hRX ⟨z,hzs,rfl⟩,hRV ⟨z,hzs,rfl⟩⟩ end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence end end section /-! # The linear hot transport equation for the actual extracted cap limit Mixed cold-hot convergence identifies the collision source. Compactness and Carleman hypotheses give the linear transport equation for the extracted limit. -/ noncomputable section open MeasureTheory Filter Set open scoped Topology ENNReal open BoltzmannNonuniqueness.TransportCutoff BoltzmannNonuniqueness.CollisionCompactness namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q} {S : AttainedCapSequence F} theorem HotPairExtraction.separated_transport_balance (hDP : Published.DunfordPettis1940HotPairWindows) (hcarleman : Published.GPV2009CarlemanInput) (hGLPS : Published.GLPS1988Proposition3) (E : HotPairExtraction S) (hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2) (hK : 0 ≤ K) (hα : 0 < α) (hαmax : α ≤ 1/4) (hγ : 0 < γ) (hd₀ : 0 < d₀) (hd₀max : d₀ ≤ 1) (hsmall : JetComparisonCoefficient.coefficient K*d₀*s₀^9 ≤ 1) (hq₁ : 1 < q) (hq₂ : q < 2) {a A B R Rₑ : ℝ} (ha : 0 < a) (haA : a ≤ A) (hAB : A < B) (hB : ENNReal.ofReal B < E.horizon) (hR : 0 ≤ R) {χ : Published.KineticPhase → ℝ} (hχ : ContDiff ℝ (⊤ : ℕ∞) χ) (hc : HasCompactSupport χ) (hs : tsupport χ ⊆ kineticWindow a A Rₑ) (hsC : ∀ z ∈ tsupport χ, EuclideanFlight.hotChart z ∈ coldCylinderSet a A R) {θ : ℝ × JetPrototype.Space → ℝ} (hθ : Measurable θ) {Cθ : ℝ} (hθB : ∀ x, |θ x| ≤ Cθ) {φ : Velocity → ℝ} (hφ : Continuous φ) {Cφ : ℝ} (hφB : ∀ v, |φ v| ≤ Cφ) (hsep : ∀ z, χ (EuclideanFlight.hotChart.symm z) = θ z.1*φ z.2) : (∫ z, transportDerivative χ (EuclideanFlight.hotChart.symm z)*E.hotLimit z ∂(coldCylinderVolume a A R).prod volume) + (2*(∫ z, θ z.1*incomingGainTest φ z.2 ∂E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))- (∫ z, θ z.1*incomingLossTest φ z.2 ∂E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))) = 0 := by have hA : ENNReal.ofReal A < E.horizon := (ENNReal.ofReal_le_ofReal hAB.le).trans_lt hB obtain ⟨κ,hκ,hsource⟩ := E.hot_source_weak_limit hDP hcarleman hGLPS hs₀ hsmax hη hηmax hK hα hαmax hγ hd₀ hd₀max hsmall hq₁ hq₂ let μ := (coldCylinderVolume a A R).prod (volume : Measure Velocity) let D : HotKineticPhase → ℝ := fun z => transportDerivative χ (EuclideanFlight.hotChart.symm z) have hDm : Measurable D := (transportDerivative_continuous hχ).measurable.comp EuclideanFlight.hotChart.symm.measurable obtain ⟨CD,hDb⟩ := (transportDerivative_continuous hχ).bounded_above_of_compact_support (transportDerivative_hasCompactSupport hc) have hDB (z) : |D z| ≤ CD := hDb _ have hlimF := ((E.toHotLimitExtraction.physical_weak_cylinder S hs₀ ha.le hA R).2.2 D hDm ⟨CD,hDB⟩).comp hκ.tendsto_atTop have hlimQ := hsource a A R ha haA hA hR θ hθ Cθ hθB φ hφ Cφ hφB have hlim := hlimF.add hlimQ have hψ : Measurable (fun z : HotKineticPhase => θ z.1*φ z.2) := (hθ.comp measurable_fst).mul (hφ.measurable.comp measurable_snd) have hCθ : 0 ≤ Cθ := (abs_nonneg (θ (0,0))).trans (hθB _) have hψB (z : HotKineticPhase) : |θ z.1*φ z.2| ≤ Cθ*Cφ := by rw [abs_mul] exact mul_le_mul (hθB _) (hφB _) (abs_nonneg _) hCθ have he : (fun n => (∫ z, D z*S.physicalHotDensity (E.indices (κ n)) z ∂μ)+ (∫ z, (θ z.1*φ z.2)*S.hotSourceDensity a A (E.indices (κ n)) z ∂μ)) =ᶠ[atTop] (fun _ => (0 : ℝ)) := by filter_upwards [hκ.tendsto_atTop.eventually (S.eventually_physicalHot_cylinder_integrable E.toHotLimitExtraction hs₀ hsmax hη hηmax hK hd₀.le hq₂ ha.le hA R), S.eventually_hotSource_cylinder_integrable hcarleman hs₀ hsmax hη hηmax hK hα (hαmax.trans (by norm_num)) hγ hd₀ hd₀max hsmall hq₁ hq₂ (E.indices_strict.comp hκ) (E.horizon_limit.comp hκ.tendsto_atTop) ha haA hA R, S.eventually_hot_transport_balance hcarleman hs₀ hsmax hη hηmax hK hα (hαmax.trans (by norm_num)) hγ hd₀ hd₀max hsmall hq₁ hq₂ (E.indices_strict.comp hκ) (E.horizon_limit.comp hκ.tendsto_atTop) ha haA hAB hB hχ hc hs] with n hfi hqi hbal have hiF := hfi.bdd_mul hDm.aestronglyMeasurable (ae_of_all _ hDB) have hiQ := hqi.bdd_mul hψ.aestronglyMeasurable (ae_of_all _ hψB) dsimp only [μ,Function.comp_def] at hiQ ⊢ rw [← integral_add hiF hiQ] have hb := S.hot_transport_cylinder_of_balance (E.indices (κ n)) hsC hbal simpa only [D,μ,hsep] using hb exact tendsto_nhds_unique hlim (tendsto_const_nhds.congr' he.symm) end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence end end section /-! # The actual hot source limit for every compact continuous kinetic test -/ noncomputable section open MeasureTheory Filter open scoped Topology ENNReal open BoltzmannNonuniqueness.CollisionCompactness namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q} {S : AttainedCapSequence F} theorem HotPairExtraction.hot_source_compact_limit (hDP : Published.DunfordPettis1940HotPairWindows) (hcarleman : Published.GPV2009CarlemanInput) (hGLPS : Published.GLPS1988Proposition3) (E : HotPairExtraction S) (hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2) (hK : 0 ≤ K) (hα : 0 < α) (hαmax : α ≤ 1/4) (hγ : 0 < γ) (hd₀ : 0 < d₀) (hd₀max : d₀ ≤ 1) (hsmall : JetComparisonCoefficient.coefficient K*d₀*s₀^9 ≤ 1) (hq₁ : 1 < q) (hq₂ : q < 2) : ∃ κ : ℕ → ℕ, StrictMono κ ∧ ∀ a A R : ℝ, ∀ ha : 0 < a, a ≤ A → ENNReal.ofReal A < E.horizon → 0 ≤ R → ∀ ψ : C(HotKineticPhase,ℝ), HasCompactSupport ψ → Tendsto (fun n => ∫ z, ψ z*S.hotSourceDensity a A (E.indices (κ n)) z ∂(coldCylinderVolume a A R).prod volume) atTop (𝓝 (2*(∫ z, ψ z ∂incomingGainMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))- (∫ z, ψ z ∂incomingLossMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))))) := by obtain ⟨κ,hκ,herr⟩ := E.vanishing_physical_collision_error hDP hcarleman hGLPS hs₀ hsmax hη hηmax hK hα (hαmax.trans (by norm_num)) hγ hd₀ hd₀max hsmall hq₁ hq₂ refine ⟨κ,hκ,fun a A R ha haA hA hR ψ hc => ?_⟩ obtain ⟨B,hB⟩ := ψ.continuous.bounded_above_of_compact_support hc have hB0 : 0 ≤ B := (abs_nonneg (ψ 0)).trans (hB _) have he := Compactness.bounded_test_integral_tendsto_zero (fun n => (S.physicalCollisionError_measurable hs₀ hsmax hη hηmax hK hd₀.le hq₂ a A (E.indices (κ n))).aestronglyMeasurable) (herr a A R ha haA hA) ψ.continuous.measurable hB0 hB have hg := (E.gain_measure_compact_limit hcarleman hGLPS hs₀ hsmax hη hηmax hK hα hαmax hγ hd₀ hd₀max hsmall hq₁ hq₂ ha haA hA hR ψ hc).comp hκ.tendsto_atTop have hl := (E.loss_measure_compact_limit hcarleman hGLPS hs₀ hsmax hη hηmax hK hα hαmax hγ hd₀ hd₀max hsmall hq₁ hq₂ ha haA hA hR ψ hc).comp hκ.tendsto_atTop have ht := ((hg.const_mul 2).sub hl).add he simp only [add_zero] at ht apply ht.congr' have hei : ∀ᶠ n in atTop, Integrable (S.physicalCollisionError a A (E.indices (κ n))) ((coldCylinderVolume a A R).prod volume) := ((herr a A R ha haA hA).eventually (eventually_lt_nhds (show (0 : ℝ≥0∞) < ⊤ from ENNReal.coe_lt_top))).mono (fun _ hn => memLp_one_iff_integrable.mp hn) filter_upwards [S.eventually_hot_source_error_identity hcarleman hs₀ hsmax hη hηmax hK hd₀.le hq₁ hq₂ (E.horizon_limit.comp hκ.tendsto_atTop) (R := R) ha.le hA, S.eventually_mixedPreRate_integrable hs₀ hsmax hη hηmax hK hα (hαmax.trans (by norm_num)) hγ hd₀ hd₀max hsmall hq₂ (E.indices_strict.comp hκ) (E.horizon_limit.comp hκ.tendsto_atTop) (R := R) ha haA hA,hei] with n hn hpre hei dsimp only [Function.comp_def] at hpre have hp := hpre (S.collisionCutoff (E.indices (κ n))) have hcold := fun p => (S.rescaledColdDensity_bounds hs₀ hsmax hη hηmax hK hd₀.le hq₂ (E.indices (κ n)) p).1 have hhot := S.hotDensity_nonneg hs₀ hsmax hη hηmax hK hd₀.le hq₂ (E.indices (κ n)) have hgi := mixed_gain_test_integrable hp ψ.continuous.measurable hB have hli := (mixedLossDensity_integrable hp).bdd_mul ψ.continuous.aestronglyMeasurable (ae_of_all _ hB) have heψ := hei.bdd_mul ψ.continuous.aestronglyMeasurable (ae_of_all _ hB) dsimp only [Function.comp_def,physicalGainMeasure,physicalLossMeasure] rw [mixedGainMeasure_integral hcold hhot hp ψ,mixedLossMeasure_integral hcold hhot hp ψ, ← integral_const_mul,← integral_sub (hgi.const_mul 2) hli] have hsub := (hgi.const_mul 2).sub hli change Integrable (fun z => (2 : ℝ)*(ψ z*_) - ψ z*_) _ at hsub rw [← integral_add hsub heψ] apply integral_congr_ae filter_upwards [hn,mixed_loss_ae_eq_frequency hp] with z hz hlz rw [hz,hlz] change _ = ψ z*(2*mixedGainDensity (S.collisionCutoff (E.indices (κ n))) (S.rescaledColdDensity (E.indices (κ n))) (S.hotDensity (E.indices (κ n))) z- S.hotDensity (E.indices (κ n)) z*KineticCollisionNullSets.frequency (S.collisionCutoff (E.indices (κ n))) (S.rescaledColdDensity (E.indices (κ n))) z+ S.physicalCollisionError a A (E.indices (κ n)) z) ring end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence end end section /-! # The actual limiting hot equation for every smooth compact kinetic test Mixed cold-hot convergence identifies the collision source. Compactness and Carleman hypotheses give the transport equation for the extracted limit. -/ noncomputable section open MeasureTheory Filter Set open scoped Topology ENNReal open BoltzmannNonuniqueness.TransportCutoff BoltzmannNonuniqueness.CollisionCompactness namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q} {S : AttainedCapSequence F} theorem HotPairExtraction.transport_measure_balance (hDP : Published.DunfordPettis1940HotPairWindows) (hcarleman : Published.GPV2009CarlemanInput) (hGLPS : Published.GLPS1988Proposition3) (E : HotPairExtraction S) (hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2) (hK : 0 ≤ K) (hα : 0 < α) (hαmax : α ≤ 1/4) (hγ : 0 < γ) (hd₀ : 0 < d₀) (hd₀max : d₀ ≤ 1) (hsmall : JetComparisonCoefficient.coefficient K*d₀*s₀^9 ≤ 1) (hq₁ : 1 < q) (hq₂ : q < 2) {a A B R Rₑ : ℝ} (ha : 0 < a) (haA : a ≤ A) (hAB : A < B) (hB : ENNReal.ofReal B < E.horizon) (hR : 0 ≤ R) {χ : Published.KineticPhase → ℝ} (hχ : ContDiff ℝ (⊤ : ℕ∞) χ) (hc : HasCompactSupport χ) (hs : tsupport χ ⊆ kineticWindow a A Rₑ) (hsC : ∀ z ∈ tsupport χ, EuclideanFlight.hotChart z ∈ coldCylinderSet a A R) : (∫ z, transportDerivative χ (EuclideanFlight.hotChart.symm z)*E.hotLimit z ∂(coldCylinderVolume a A R).prod volume) + (2*(∫ z, χ (EuclideanFlight.hotChart.symm z) ∂incomingGainMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))- (∫ z, χ (EuclideanFlight.hotChart.symm z) ∂incomingLossMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))) = 0 := by have hA : ENNReal.ofReal A < E.horizon := (ENNReal.ofReal_le_ofReal hAB.le).trans_lt hB obtain ⟨κ,hκ,hsource⟩ := E.hot_source_compact_limit hDP hcarleman hGLPS hs₀ hsmax hη hηmax hK hα hαmax hγ hd₀ hd₀max hsmall hq₁ hq₂ let μ := (coldCylinderVolume a A R).prod (volume : Measure Velocity) let D : HotKineticPhase → ℝ := fun z => transportDerivative χ (EuclideanFlight.hotChart.symm z) have hDm : Measurable D := (transportDerivative_continuous hχ).measurable.comp EuclideanFlight.hotChart.symm.measurable obtain ⟨CD,hDb⟩ := (transportDerivative_continuous hχ).bounded_above_of_compact_support (transportDerivative_hasCompactSupport hc) have hDB (z) : |D z| ≤ CD := hDb _ have hlimF := ((E.toHotLimitExtraction.physical_weak_cylinder S hs₀ ha.le hA R).2.2 D hDm ⟨CD,hDB⟩).comp hκ.tendsto_atTop let ψ : C(HotKineticPhase,ℝ) := ⟨fun z => χ (EuclideanFlight.hotChart.symm z), hχ.continuous.comp EuclideanFlight.hotChart_symm_continuous⟩ have hlimQ := hsource a A R ha haA hA hR ψ (EuclideanFlight.compact_test_hotChart hc) have hlim := hlimF.add hlimQ obtain ⟨Cψ,hψB⟩ := ψ.continuous.bounded_above_of_compact_support (EuclideanFlight.compact_test_hotChart hc) have he : (fun n => (∫ z, D z*S.physicalHotDensity (E.indices (κ n)) z ∂μ)+ (∫ z, ψ z*S.hotSourceDensity a A (E.indices (κ n)) z ∂μ)) =ᶠ[atTop] (fun _ => (0 : ℝ)) := by filter_upwards [hκ.tendsto_atTop.eventually (S.eventually_physicalHot_cylinder_integrable E.toHotLimitExtraction hs₀ hsmax hη hηmax hK hd₀.le hq₂ ha.le hA R), S.eventually_hotSource_cylinder_integrable hcarleman hs₀ hsmax hη hηmax hK hα (hαmax.trans (by norm_num)) hγ hd₀ hd₀max hsmall hq₁ hq₂ (E.indices_strict.comp hκ) (E.horizon_limit.comp hκ.tendsto_atTop) ha haA hA R, S.eventually_hot_transport_balance hcarleman hs₀ hsmax hη hηmax hK hα (hαmax.trans (by norm_num)) hγ hd₀ hd₀max hsmall hq₁ hq₂ (E.indices_strict.comp hκ) (E.horizon_limit.comp hκ.tendsto_atTop) ha haA hAB hB hχ hc hs] with n hfi hqi hbal have hiF := hfi.bdd_mul hDm.aestronglyMeasurable (ae_of_all _ hDB) have hiQ := hqi.bdd_mul ψ.continuous.aestronglyMeasurable (ae_of_all _ hψB) dsimp only [μ,Function.comp_def] at hiQ ⊢ rw [← integral_add hiF hiQ] have hb := S.hot_transport_cylinder_of_balance (E.indices (κ n)) hsC hbal simpa only [D,μ,ψ,ContinuousMap.coe_mk] using hb exact tendsto_nhds_unique hlim (tendsto_const_nhds.congr' he.symm) end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence end end section /-! # Exact periodicity of the cap hot remainder and its bounded ratio -/ noncomputable section open MeasureTheory open BoltzmannNonuniqueness.WeightedTranslation BoltzmannNonuniqueness.WeightedLocal open BoltzmannNonuniqueness.WeightedLocalControl BoltzmannNonuniqueness.VelocityWeight namespace BoltzmannNonuniqueness.JetCopyDatum theorem CapApproximation.hot_periodic {s₀ η K α γ d₀ q T : ℝ} {N : ℕ} (F : CapApproximation s₀ η K α γ d₀ q T N) (k : JetLattice.Lattice) : pull (displacement k) F.hot = F.hot := by funext u change F.solution.value (u.1,shift (displacement k) u.2)- (∑' i, rebuilt s₀ η K α γ d₀ q (N+1) (damping q (N+1) F.amplitude) T N F.solution.value i (u.1,shift (displacement k) u.2)) = _ have hs := congrFun (F.solution.periodic k) u have hc (i : JetLattice.Label) := congrFun (rebuilt_shift (s₀ := s₀) (η := η) (K := K) (α := α) (γ := γ) (d₀ := d₀) (q := q) (b := N+1) (L := damping q (N+1) F.amplitude) (T := T) (N := N) k (F.solution.periodic k) i) u change F.solution.value (u.1,shift (displacement k) u.2) = F.solution.value u at hs simp only [pull] at hc rw [hs] simp_rw [hc] exact congrArg (fun c => F.solution.value u-c) ((relabel k).tsum_eq (fun i => rebuilt s₀ η K α γ d₀ q (N+1) (damping q (N+1) F.amplitude) T N F.solution.value i u)) namespace AttainedCapSequence variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q} theorem euclideanHot_div_weight (S : AttainedCapSequence F) (n : ℕ) (z : Published.KineticPhase) : S.euclideanHot n z/H q z.2 = (F.approximation n).hot (S.radius n*z.1.1,(S.radius n • JetPeriodicDatum.spatialMap z.1.2,z.2))/S.radius n := by rw [euclideanHot_eq_rescaledHot,rescaledHot_eq_weighted] simp only [EuclideanFlight.phaseEquiv_apply,JetPeriodicDatum.phaseMap] rw [mul_div_cancel_left₀ _ (H_pos q z.2).ne'] rfl theorem boundedHotRatio_periodic (S : AttainedCapSequence F) (hs₀ : 0 < s₀) (n : ℕ) (t : ℝ) (k : JetLattice.Lattice) (p : Velocity × Velocity) : S.boundedHotRatio n ((t,p.1-(S.radius n)⁻¹ • latticeVector k),p.2) = S.boundedHotRatio n ((t,p.1),p.2) := by unfold boundedHotRatio rw [euclideanHot_div_weight,euclideanHot_div_weight] have he : S.radius n • JetPeriodicDatum.spatialMap (p.1-(S.radius n)⁻¹ • latticeVector k) = S.radius n • JetPeriodicDatum.spatialMap p.1-displacement k := by apply Prod.ext · ext i change S.radius n*(p.1 i.castSucc-(S.radius n)⁻¹*(k i.castSucc:ℝ)) = S.radius n*p.1 i.castSucc-(k i.castSucc:ℝ) field_simp [(S.radius_pos hs₀ n).ne'] · change S.radius n*(p.1 (Fin.last 2)-(S.radius n)⁻¹*(k (Fin.last 2):ℝ)) = S.radius n*p.1 (Fin.last 2)-(k (Fin.last 2):ℝ) field_simp [(S.radius_pos hs₀ n).ne'] rw [he] have hp := congrFun ((F.approximation n).hot_periodic k) (S.radius n*t,(S.radius n • JetPeriodicDatum.spatialMap p.1,p.2)) change (F.approximation n).hot (S.radius n*t,(S.radius n • JetPeriodicDatum.spatialMap p.1-displacement k,p.2)) = _ at hp rw [hp] end AttainedCapSequence end BoltzmannNonuniqueness.JetCopyDatum end end section /-! # The actual limiting transport equation with its loss attenuation -/ noncomputable section open MeasureTheory Set open scoped ENNReal open BoltzmannNonuniqueness.TransportCutoff BoltzmannNonuniqueness.CollisionCompactness namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q} {S : AttainedCapSequence F} theorem HotPairExtraction.attenuated_transport_balance (hDP : Published.DunfordPettis1940HotPairWindows) (hcarleman : Published.GPV2009CarlemanInput) (hGLPS : Published.GLPS1988Proposition3) (E : HotPairExtraction S) (hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2) (hK : 0 ≤ K) (hα : 0 < α) (hαmax : α ≤ 1/4) (hγ : 0 < γ) (hd₀ : 0 < d₀) (hd₀max : d₀ ≤ 1) (hsmall : JetComparisonCoefficient.coefficient K*d₀*s₀^9 ≤ 1) (hq₁ : 1 < q) (hq₂ : q < 2) {a A B R Rₑ : ℝ} (ha : 0 < a) (haA : a ≤ A) (hAB : A < B) (hB : ENNReal.ofReal B < E.horizon) (hR : 0 ≤ R) {χ : Published.KineticPhase → ℝ} (hχ : ContDiff ℝ (⊤ : ℕ∞) χ) (hc : HasCompactSupport χ) (hs : tsupport χ ⊆ kineticWindow a A Rₑ) (hsC : ∀ z ∈ tsupport χ, EuclideanFlight.hotChart z ∈ coldCylinderSet a A R) : (∫ z, (transportDerivative χ (EuclideanFlight.hotChart.symm z)- χ (EuclideanFlight.hotChart.symm z)*GeometricBackground.frequency E.phase η E.fraction K α γ z.1.1 z.1.2 z.2)*E.hotLimit z ∂(coldCylinderVolume a A R).prod volume)+ 2*(∫ z, χ (EuclideanFlight.hotChart.symm z) ∂incomingGainMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))) = 0 := by have hA : ENNReal.ofReal A < E.horizon := (ENNReal.ofReal_le_ofReal hAB.le).trans_lt hB have hb := E.transport_measure_balance hDP hcarleman hGLPS hs₀ hsmax hη hηmax hK hα hαmax hγ hd₀ hd₀max hsmall hq₁ hq₂ ha haA hAB hB hR hχ hc hs hsC let ψ : HotKineticPhase → ℝ := fun z => χ (EuclideanFlight.hotChart.symm z) have hψ : Measurable ψ := hχ.continuous.measurable.comp EuclideanFlight.hotChart.symm.measurable obtain ⟨Cψ,hψB⟩ := hχ.continuous.bounded_above_of_compact_support hc have hψBound (z) : |ψ z| ≤ Cψ := hψB _ rw [E.toHotLimitExtraction.actual_loss_cylinder_integral ha haA hK hα hγ hq₂ hψ hψBound] at hb obtain ⟨CD,hDB⟩ := (transportDerivative_continuous hχ).bounded_above_of_compact_support (transportDerivative_hasCompactSupport hc) have hd := ((E.toHotLimitExtraction.physical_weak_cylinder S hs₀ ha.le hA R).2.1).bdd_mul ((transportDerivative_continuous hχ).measurable.comp EuclideanFlight.hotChart.symm.measurable).aestronglyMeasurable (ae_of_all _ (fun z => hDB (EuclideanFlight.hotChart.symm z))) dsimp only [Function.comp_def] at hd have hl := (E.toHotLimitExtraction.actual_loss_cylinder_integrable (R := R) ha haA hK hα hγ hq₂).bdd_mul hψ.aestronglyMeasurable (ae_of_all _ hψBound) have he : (∫ z, (transportDerivative χ (EuclideanFlight.hotChart.symm z)- ψ z*GeometricBackground.frequency E.phase η E.fraction K α γ z.1.1 z.1.2 z.2)* E.hotLimit z ∂(coldCylinderVolume a A R).prod volume) = (∫ z, transportDerivative χ (EuclideanFlight.hotChart.symm z)*E.hotLimit z ∂(coldCylinderVolume a A R).prod volume)- (∫ z, ψ z*(E.hotLimit z*GeometricBackground.frequency E.phase η E.fraction K α γ z.1.1 z.1.2 z.2) ∂(coldCylinderVolume a A R).prod volume) := by rw [← integral_sub hd hl] apply integral_congr_ae exact ae_of_all _ (fun z => by ring) change (∫ z, (transportDerivative χ (EuclideanFlight.hotChart.symm z)- ψ z*GeometricBackground.frequency E.phase η E.fraction K α γ z.1.1 z.1.2 z.2)* E.hotLimit z ∂(coldCylinderVolume a A R).prod volume)+_ = 0 rw [he] linarith end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence end end section /-! # The actual hot transport equation with finite incoming gain and loss measures -/ noncomputable section open MeasureTheory Filter Set open scoped ENNReal open BoltzmannNonuniqueness.TransportCutoff BoltzmannNonuniqueness.CollisionCompactness namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q} {S : AttainedCapSequence F} theorem HotPairExtraction.separated_transport_measure_balance (hDP : Published.DunfordPettis1940HotPairWindows) (hcarleman : Published.GPV2009CarlemanInput) (hGLPS : Published.GLPS1988Proposition3) (E : HotPairExtraction S) (hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2) (hK : 0 ≤ K) (hα : 0 < α) (hαmax : α ≤ 1/4) (hγ : 0 < γ) (hd₀ : 0 < d₀) (hd₀max : d₀ ≤ 1) (hsmall : JetComparisonCoefficient.coefficient K*d₀*s₀^9 ≤ 1) (hq₁ : 1 < q) (hq₂ : q < 2) {a A B R Rₑ : ℝ} (ha : 0 < a) (haA : a ≤ A) (hAB : A < B) (hB : ENNReal.ofReal B < E.horizon) (hR : 0 ≤ R) {χ : Published.KineticPhase → ℝ} (hχ : ContDiff ℝ (⊤ : ℕ∞) χ) (hc : HasCompactSupport χ) (hs : tsupport χ ⊆ kineticWindow a A Rₑ) (hsC : ∀ z ∈ tsupport χ, EuclideanFlight.hotChart z ∈ coldCylinderSet a A R) {θ : ℝ × JetPrototype.Space → ℝ} (hθ : Measurable θ) {Cθ : ℝ} (hθB : ∀ x, |θ x| ≤ Cθ) {φ : Velocity → ℝ} (hφ : Continuous φ) {Cφ : ℝ} (hφB : ∀ v, |φ v| ≤ Cφ) (hsep : ∀ z, χ (EuclideanFlight.hotChart.symm z) = θ z.1*φ z.2) : (∫ z, transportDerivative χ (EuclideanFlight.hotChart.symm z)*E.hotLimit z ∂(coldCylinderVolume a A R).prod volume)+ 2*(∫ z, χ (EuclideanFlight.hotChart.symm z) ∂incomingGainMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))- (∫ z, χ (EuclideanFlight.hotChart.symm z) ∂incomingLossMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))) = 0 := by let μ := E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R) let _ : SFinite μ := by dsimp [μ,HotLimitExtraction.mixedMeasure]; infer_instance have hi : Integrable incomingRate μ := E.toHotLimitExtraction.incomingRate_integrable ha (ha.le.trans haA) hK hα hγ hq₂ have hCθ : 0 ≤ Cθ := (abs_nonneg (θ (0,0))).trans (hθB _) have hg := incomingGainMeasure_separated hi hθ hCθ hθB hφ.measurable hφB have hl := incomingLossMeasure_separated hi hθ hCθ hθB hφ.measurable hφB simp_rw [hsep] change _+2*(∫ z, θ z.1*φ z.2 ∂incomingGainMeasure μ)- (∫ z, θ z.1*φ z.2 ∂incomingLossMeasure μ) = 0 rw [hg,hl] have hb := E.separated_transport_balance hDP hcarleman hGLPS hs₀ hsmax hη hηmax hK hα hαmax hγ hd₀ hd₀max hsmall hq₁ hq₂ ha haA hAB hB hR hχ hc hs hsC hθ hθB hφ hφB hsep dsimp only [μ] at hg hl ⊢ linarith end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence end end section /-! # The actual hot-limit equation tested in characteristic coordinates -/ noncomputable section open MeasureTheory Set open scoped ENNReal open BoltzmannNonuniqueness.TransportCutoff BoltzmannNonuniqueness.CollisionCompactness namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q} {S : AttainedCapSequence F} theorem HotPairExtraction.characteristic_test_balance (hDP : Published.DunfordPettis1940HotPairWindows) (hcarleman : Published.GPV2009CarlemanInput) (hGLPS : Published.GLPS1988Proposition3) (E : HotPairExtraction S) (hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2) (hK : 0 ≤ K) (hα : 0 < α) (hαmax : α ≤ 1/4) (hγ : 0 < γ) (hd₀ : 0 < d₀) (hd₀max : d₀ ≤ 1) (hsmall : JetComparisonCoefficient.coefficient K*d₀*s₀^9 ≤ 1) (hq₁ : 1 < q) (hq₂ : q < 2) {a A B R Rₑ : ℝ} (ha : 0 < a) (haA : a ≤ A) (hAB : A < B) (hB : ENNReal.ofReal B < E.horizon) (hR : 0 ≤ R) {ψ : EuclideanFlight.CharacteristicPhase → ℝ} (hψ : ContDiff ℝ (⊤ : ℕ∞) ψ) (hc : HasCompactSupport ψ) (hs : tsupport (EuclideanFlight.testPullback ψ) ⊆ kineticWindow a A Rₑ) (hsC : ∀ z ∈ tsupport (EuclideanFlight.testPullback ψ), EuclideanFlight.hotChart z ∈ coldCylinderSet a A R) : (∫ z, EuclideanFlight.timeDerivative ψ (EuclideanFlight.characteristicEquiv.symm (EuclideanFlight.hotChart.symm z))*E.hotLimit z ∂(coldCylinderVolume a A R).prod volume)+ (2*(∫ z, ψ (EuclideanFlight.characteristicEquiv.symm (EuclideanFlight.hotChart.symm z)) ∂incomingGainMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))- (∫ z, ψ (EuclideanFlight.characteristicEquiv.symm (EuclideanFlight.hotChart.symm z)) ∂incomingLossMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))) = 0 := by have hb := E.transport_measure_balance hDP hcarleman hGLPS hs₀ hsmax hη hηmax hK hα hαmax hγ hd₀ hd₀max hsmall hq₁ hq₂ ha haA hAB hB hR (EuclideanFlight.testPullback_contDiff hψ) (EuclideanFlight.testPullback_compact hc) hs hsC simp_rw [EuclideanFlight.transportDerivative_testPullback hψ] at hb exact hb end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence end end section /-! # Cumulative collision balance for the actual weak hot limit Every smooth nonnegative compact phase test has an almost-everywhere time trace given by a constant and the cumulative incoming gain minus incoming loss. Both source measures are built from the actual mixed atomic-cold/hot measure. -/ noncomputable section open MeasureTheory Set open scoped NNReal ENNReal open BoltzmannNonuniqueness.CollisionCompactness BoltzmannNonuniqueness.EuclideanFlight namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q} {S : AttainedCapSequence F} def HotLimitExtraction.characteristicGainMeasure (E : HotLimitExtraction S) {a : ℝ} (ha : 0 < a) (hK : 0 ≤ K) (hα : 0 < α) (hγ : 0 < γ) (A R : ℝ) : Measure CharacteristicPhase := (2 : ℝ≥0) • sourcePullback (incomingGainMeasure (E.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))) def HotLimitExtraction.characteristicLossMeasure (E : HotLimitExtraction S) {a : ℝ} (ha : 0 < a) (hK : 0 ≤ K) (hα : 0 < α) (hγ : 0 < γ) (A R : ℝ) : Measure CharacteristicPhase := sourcePullback (incomingLossMeasure (E.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))) theorem HotPairExtraction.characteristic_cumulative_balance (hDP : Published.DunfordPettis1940HotPairWindows) (hcarleman : Published.GPV2009CarlemanInput) (hGLPS : Published.GLPS1988Proposition3) (E : HotPairExtraction S) (hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2) (hK : 0 ≤ K) (hα : 0 < α) (hαmax : α ≤ 1/4) (hγ : 0 < γ) (hd₀ : 0 < d₀) (hd₀max : d₀ ≤ 1) (hsmall : JetComparisonCoefficient.coefficient K*d₀*s₀^9 ≤ 1) (hq₁ : 1 < q) (hq₂ : q < 2) {a A B : ℝ} (ha : 0 < a) (haA : a < A) (hAB : A < B) (hB : ENNReal.ofReal B < E.horizon) {φ : Velocity × Velocity → ℝ} (hφ : ContDiff ℝ (⊤ : ℕ∞) φ) (hc : HasCompactSupport φ) (hn : ∀ p, 0 ≤ φ p) : ∃ R : ℝ, 0 ≤ R ∧ ∃ c : ℝ, ∀ᵐ t ∂volume, t ∈ Ioo a A → WeakTime.phaseProjection (cylinderPullback a A R E.hotLimit) φ t = c+WeakTime.cumulative (WeakTime.timeSource (E.toHotLimitExtraction.characteristicGainMeasure ha hK hα hγ A R) φ) t- WeakTime.cumulative (WeakTime.timeSource (E.toHotLimitExtraction.characteristicLossMeasure ha hK hα hγ A R) φ) t := by obtain ⟨R,Rₑ,hR,hloc⟩ := exists_timePhase_cylinder a A hc refine ⟨R,hR,?_⟩ let μ := E.toHotLimitExtraction.characteristicGainMeasure ha hK hα hγ A R let ν := E.toHotLimitExtraction.characteristicLossMeasure ha hK hα hγ A R let _ := E.toHotLimitExtraction.incomingGainMeasure_finite (R := R) ha (ha.le.trans haA.le) hK hα hγ hq₂ let _ := E.toHotLimitExtraction.incomingLossMeasure_finite (R := R) ha (ha.le.trans haA.le) hK hα hγ hq₂ have : IsFiniteMeasure μ := by dsimp [μ,HotLimitExtraction.characteristicGainMeasure]; infer_instance have : IsFiniteMeasure ν := by dsimp [ν,HotLimitExtraction.characteristicLossMeasure]; infer_instance obtain ⟨C,hC⟩ := hφ.continuous.bounded_above_of_compact_support hc have hi := (E.toHotLimitExtraction.physical_weak_cylinder S hs₀ ha.le ((ENNReal.ofReal_le_ofReal hAB.le).trans_lt hB) R).2.1 apply WeakTime.projected_cumulative_balance haA (cylinderPullback_integrable hi) hφ.continuous.measurable hn hC μ ν intro θ hθ hθc hθs have hlocθ := hloc θ hθs have hb := E.characteristic_test_balance hDP hcarleman hGLPS hs₀ hsmax hη hηmax hK hα hαmax hγ hd₀ hd₀max hsmall hq₁ hq₂ ha haA.le hAB hB hR (timePhaseTest_contDiff hθ hφ) (timePhaseTest_compact hθc hc) hlocθ.1 hlocθ.2 simp_rw [timeDerivative_timePhaseTest hθ hφ] at hb rw [cylinderPullback_integral] have hm : Measurable (fun z : CharacteristicPhase => θ z.1*φ z.2) := (hθ.continuous.measurable.comp measurable_fst).mul (hφ.continuous.measurable.comp measurable_snd) change _ + (∫ z, θ z.1*φ z.2 ∂((2 : ℝ≥0) • sourcePullback _))- (∫ z, θ z.1*φ z.2 ∂sourcePullback _) = 0 rw [integral_smul_nnreal_measure,sourcePullback_integral _ hm,sourcePullback_integral _ hm] change _ + 2*(∫ z, θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2 ∂incomingGainMeasure (E.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))) - _ = 0 change (∫ z, (deriv θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2)* E.hotLimit z ∂(coldCylinderVolume a A R).prod volume)+ (2*(∫ z, θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2 ∂incomingGainMeasure (E.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))- (∫ z, θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2 ∂incomingLossMeasure (E.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))) = 0 at hb linarith only [hb] end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence end end section /-! # The actual weak-balance cylinder also covers the full compact phase support -/ noncomputable section open MeasureTheory Set open scoped NNReal ENNReal open BoltzmannNonuniqueness.CollisionCompactness BoltzmannNonuniqueness.EuclideanFlight namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q} {S : AttainedCapSequence F} theorem HotPairExtraction.covered_characteristic_weak_balance (hDP : Published.DunfordPettis1940HotPairWindows) (hcarleman : Published.GPV2009CarlemanInput) (hGLPS : Published.GLPS1988Proposition3) (E : HotPairExtraction S) (hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2) (hK : 0 ≤ K) (hα : 0 < α) (hαmax : α ≤ 1/4) (hγ : 0 < γ) (hd₀ : 0 < d₀) (hd₀max : d₀ ≤ 1) (hsmall : JetComparisonCoefficient.coefficient K*d₀*s₀^9 ≤ 1) (hq₁ : 1 < q) (hq₂ : q < 2) {a A B : ℝ} (ha : 0 < a) (haA : a < A) (hAB : A < B) (hB : ENNReal.ofReal B < E.horizon) {β : Velocity × Velocity → ℝ} (hβc : HasCompactSupport β) : ∃ R : ℝ, 0 ≤ R ∧ (∀ t ∈ Icc a A, ∀ p ∈ tsupport β, hotCharacteristicEquiv (t,p) ∈ coldCylinderSet a A R) ∧ ∀ φ : WeakTime.Phase → ℝ, ContDiff ℝ (⊤ : ℕ∞) φ → HasCompactSupport φ → (∀ p, 0 ≤ φ p) → tsupport φ ⊆ tsupport β → ∀ θ : ℝ → ℝ, ContDiff ℝ (⊤ : ℕ∞) θ → HasCompactSupport θ → tsupport θ ⊆ Ioo a A → (∫ z, (deriv θ z.1*φ z.2)*cylinderPullback a A R E.hotLimit z)+ (∫ z, θ z.1*φ z.2 ∂E.toHotLimitExtraction.characteristicGainMeasure ha hK hα hγ A R)- (∫ z, θ z.1*φ z.2 ∂E.toHotLimitExtraction.characteristicLossMeasure ha hK hα hγ A R) = 0 := by obtain ⟨R₀,Rₑ,hR₀,hloc⟩ := exists_timePhase_cylinder_for_support a A hβc obtain ⟨R₁,_hR₁,hcover⟩ := exists_phase_cylinder a A hβc let R := max R₀ R₁ have hR : 0 ≤ R := hR₀.trans (le_max_left _ _) refine ⟨R,hR,?_,?_⟩ · intro t ht p hp exact coldCylinderSet_mono_radius (le_max_right _ _) (hcover t ht p hp) intro φ hφ hc _hn hφβ θ hθ hθc hθs have hlocθ := hloc φ hφβ θ hθs have hcoverθ : ∀ z ∈ tsupport (testPullback (timePhaseTest θ φ)), hotChart z ∈ coldCylinderSet a A R := fun z hz => coldCylinderSet_mono_radius (le_max_left _ _) (hlocθ.2 z hz) have hb := E.characteristic_test_balance hDP hcarleman hGLPS hs₀ hsmax hη hηmax hK hα hαmax hγ hd₀ hd₀max hsmall hq₁ hq₂ ha haA.le hAB hB hR (timePhaseTest_contDiff hθ hφ) (timePhaseTest_compact hθc hc) hlocθ.1 hcoverθ simp_rw [timeDerivative_timePhaseTest hθ hφ] at hb rw [cylinderPullback_integral] have hm : Measurable (fun z : CharacteristicPhase => θ z.1*φ z.2) := (hθ.continuous.measurable.comp measurable_fst).mul (hφ.continuous.measurable.comp measurable_snd) change _ + (∫ z, θ z.1*φ z.2 ∂((2 : ℝ≥0) • sourcePullback _))- (∫ z, θ z.1*φ z.2 ∂sourcePullback _) = 0 rw [integral_smul_nnreal_measure,sourcePullback_integral _ hm,sourcePullback_integral _ hm] change (∫ z, (deriv θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2)* E.hotLimit z ∂(coldCylinderVolume a A R).prod volume)+ (2*(∫ z, θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2 ∂incomingGainMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))))- (∫ z, θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2 ∂incomingLossMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))) = 0 change (∫ z, (deriv θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2)* E.hotLimit z ∂(coldCylinderVolume a A R).prod volume)+ ((2*(∫ z, θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2 ∂incomingGainMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))))- (∫ z, θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2 ∂incomingLossMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))) = 0 at hb linarith only [hb] end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence end end section /-! # The actual characteristic gain is the sum of both outgoing collision laws This identity uses the physical normal-collision law for the mixed measure, including its atomic cold partner. No density Carleman identity is used here. -/ noncomputable section open MeasureTheory open scoped NNReal ENNReal open BoltzmannNonuniqueness.CollisionCompactness BoltzmannNonuniqueness.EuclideanFlight namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q} {S : AttainedCapSequence F} theorem HotLimitExtraction.characteristicGain_test_integral (E : HotLimitExtraction S) {a A R : ℝ} (ha : 0 < a) (haA : a ≤ A) (hK : 0 ≤ K) (hα : 0 < α) (hγ : 0 < γ) (hq : q < 2) {ψ : CharacteristicPhase → ℝ} (hψ : Measurable ψ) {B : ℝ} (hB : ∀ u, |ψ u| ≤ B) : (∫ u, ψ u ∂E.characteristicGainMeasure ha hK hα hγ A R) = ∫ z, ψ (hotCharacteristicEquiv.symm (incomingLeft z))+ ψ (hotCharacteristicEquiv.symm (incomingRight z)) ∂incomingCollisionMeasure (E.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)) := by let μ := E.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R) let _ : SFinite μ := by dsimp [μ,HotLimitExtraction.mixedMeasure]; infer_instance have hi : Integrable incomingRate μ := E.incomingRate_integrable ha (ha.le.trans haA) hK hα hγ hq let _ := incomingCollisionMeasure_finite hi have hm : Measurable (fun z : HotKineticPhase => ψ (hotCharacteristicEquiv.symm z)) := hψ.comp hotCharacteristicEquiv.symm.measurable have hL : Integrable (fun z => ψ (hotCharacteristicEquiv.symm (incomingLeft z))) (incomingCollisionMeasure μ) := (integrable_const B).mono' (hm.comp incomingLeft_measurable).aestronglyMeasurable (ae_of_all _ (fun z => hB _)) have hR : Integrable (fun z => ψ (hotCharacteristicEquiv.symm (incomingRight z))) (incomingCollisionMeasure μ) := (integrable_const B).mono' (hm.comp incomingRight_measurable).aestronglyMeasurable (ae_of_all _ (fun z => hB _)) rw [HotLimitExtraction.characteristicGainMeasure,integral_smul_nnreal_measure, sourcePullback_integral _ hψ,incomingGainMeasure_integral hi hm (fun z => hB _)] change 2*((1/2 : ℝ)*_)=_ rw [integral_add hL hR] ring theorem HotLimitExtraction.characteristicGain_normal_integral (E : HotLimitExtraction S) {a A R : ℝ} (ha : 0 < a) (haA : a ≤ A) (hK : 0 ≤ K) (hα : 0 < α) (hγ : 0 < γ) (hq : q < 2) {ψ : CharacteristicPhase → ℝ} (hψ : Measurable ψ) {B : ℝ} (hB : ∀ u, |ψ u| ≤ B) : (∫ u, ψ u ∂E.characteristicGainMeasure ha hK hα hγ A R) = ∫ p, ∫ ω, collisionKernel p.2.1 p.2.2 ω* (ψ (hotCharacteristicEquiv.symm (incomingLeft (p,ω)))+ ψ (hotCharacteristicEquiv.symm (incomingRight (p,ω)))) ∂sphereArea ∂E.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R) := by let μ := E.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R) let _ : SFinite μ := by dsimp [μ,HotLimitExtraction.mixedMeasure]; infer_instance rw [E.characteristicGain_test_integral ha haA hK hα hγ hq hψ hB] apply incomingCollisionMeasure_integral_prod (E.incomingRate_integrable ha (ha.le.trans haA) hK hα hγ hq) · exact ((hψ.comp hotCharacteristicEquiv.symm.measurable).comp incomingLeft_measurable).add ((hψ.comp hotCharacteristicEquiv.symm.measurable).comp incomingRight_measurable) · intro z exact (abs_add_le _ _).trans ((add_le_add (hB _) (hB _)).trans_eq (two_mul B).symm) end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence end end section /-! # One physical cylinder for the actual weak balance of all local phase tests -/ noncomputable section open MeasureTheory Set open scoped NNReal ENNReal open BoltzmannNonuniqueness.CollisionCompactness BoltzmannNonuniqueness.EuclideanFlight namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q} {S : AttainedCapSequence F} theorem HotPairExtraction.common_characteristic_weak_balance (hDP : Published.DunfordPettis1940HotPairWindows) (hcarleman : Published.GPV2009CarlemanInput) (hGLPS : Published.GLPS1988Proposition3) (E : HotPairExtraction S) (hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2) (hK : 0 ≤ K) (hα : 0 < α) (hαmax : α ≤ 1/4) (hγ : 0 < γ) (hd₀ : 0 < d₀) (hd₀max : d₀ ≤ 1) (hsmall : JetComparisonCoefficient.coefficient K*d₀*s₀^9 ≤ 1) (hq₁ : 1 < q) (hq₂ : q < 2) {a A B : ℝ} (ha : 0 < a) (haA : a < A) (hAB : A < B) (hB : ENNReal.ofReal B < E.horizon) {β : Velocity × Velocity → ℝ} (hβc : HasCompactSupport β) : ∃ R : ℝ, 0 ≤ R ∧ ∀ φ : WeakTime.Phase → ℝ, ContDiff ℝ (⊤ : ℕ∞) φ → HasCompactSupport φ → (∀ p, 0 ≤ φ p) → tsupport φ ⊆ tsupport β → ∀ θ : ℝ → ℝ, ContDiff ℝ (⊤ : ℕ∞) θ → HasCompactSupport θ → tsupport θ ⊆ Ioo a A → (∫ z, (deriv θ z.1*φ z.2)*cylinderPullback a A R E.hotLimit z)+ (∫ z, θ z.1*φ z.2 ∂E.toHotLimitExtraction.characteristicGainMeasure ha hK hα hγ A R)- (∫ z, θ z.1*φ z.2 ∂E.toHotLimitExtraction.characteristicLossMeasure ha hK hα hγ A R) = 0 := by obtain ⟨R,Rₑ,hR,hloc⟩ := exists_timePhase_cylinder_for_support a A hβc refine ⟨R,hR,?_⟩ intro φ hφ hc _hn hφβ θ hθ hθc hθs have hlocθ := hloc φ hφβ θ hθs have hb := E.characteristic_test_balance hDP hcarleman hGLPS hs₀ hsmax hη hηmax hK hα hαmax hγ hd₀ hd₀max hsmall hq₁ hq₂ ha haA.le hAB hB hR (timePhaseTest_contDiff hθ hφ) (timePhaseTest_compact hθc hc) hlocθ.1 hlocθ.2 simp_rw [timeDerivative_timePhaseTest hθ hφ] at hb rw [cylinderPullback_integral] have hm : Measurable (fun z : CharacteristicPhase => θ z.1*φ z.2) := (hθ.continuous.measurable.comp measurable_fst).mul (hφ.continuous.measurable.comp measurable_snd) change _ + (∫ z, θ z.1*φ z.2 ∂((2 : ℝ≥0) • sourcePullback _))- (∫ z, θ z.1*φ z.2 ∂sourcePullback _) = 0 rw [integral_smul_nnreal_measure,sourcePullback_integral _ hm,sourcePullback_integral _ hm] change (∫ z, (deriv θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2)* E.hotLimit z ∂(coldCylinderVolume a A R).prod volume)+ (2*(∫ z, θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2 ∂incomingGainMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))))- (∫ z, θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2 ∂incomingLossMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))) = 0 change (∫ z, (deriv θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2)* E.hotLimit z ∂(coldCylinderVolume a A R).prod volume)+ ((2*(∫ z, θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2 ∂incomingGainMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))))- (∫ z, θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2 ∂incomingLossMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))) = 0 at hb linarith only [hb] end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence end end section /-! # The actual characteristic gain as a hot-particle and cold-partner integral -/ noncomputable section open MeasureTheory ProbabilityTheory open scoped ProbabilityTheory open BoltzmannNonuniqueness.CollisionCompactness BoltzmannNonuniqueness.EuclideanFlight namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q} {S : AttainedCapSequence F} theorem HotLimitExtraction.characteristicGain_hot_integral (E : HotLimitExtraction S) {a A R : ℝ} (ha : 0 < a) (haA : a ≤ A) (hK : 0 ≤ K) (hα : 0 < α) (hγ : 0 < γ) (hq : q < 2) {ψ : CharacteristicPhase → ℝ} (hψ : Measurable ψ) {B : ℝ} (hB : ∀ u, |ψ u| ≤ B) : (∫ u, ψ u ∂E.characteristicGainMeasure ha hK hα hγ A R) = ∫ x, ∫ w, E.cappedHot (x,w)* (∫ v, ∫ ω, collisionKernel v w ω* (ψ (hotCharacteristicEquiv.symm (x,scatterLeft v w ω))+ ψ (hotCharacteristicEquiv.symm (x,scatterRight v w ω))) ∂sphereArea ∂E.background (max a x.1) x.2) ∂volume ∂coldCylinderVolume a A R := by let μ := E.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R) let _ : SFinite μ := by dsimp [μ,HotLimitExtraction.mixedMeasure]; infer_instance let f : ((ℝ × JetPrototype.Space) × (Velocity × Velocity)) × Sphere → ℝ := fun z => ψ (hotCharacteristicEquiv.symm (incomingLeft z))+ ψ (hotCharacteristicEquiv.symm (incomingRight z)) have hm : Measurable f := ((hψ.comp hotCharacteristicEquiv.symm.measurable).comp incomingLeft_measurable).add ((hψ.comp hotCharacteristicEquiv.symm.measurable).comp incomingRight_measurable) have hb (z) : |f z| ≤ 2*B := (abs_add_le _ _).trans ((add_le_add (hB _) (hB _)).trans_eq (two_mul B).symm) have hi := incomingCollision_weight_integrable (E.incomingRate_integrable (R := R) ha (ha.le.trans haA) hK hα hγ hq) hm hb have hF : Integrable (fun p => ∫ ω, collisionKernel p.2.1 p.2.2 ω*f (p,ω) ∂sphereArea) μ := hi.integral_prod_left rw [E.characteristicGain_normal_integral ha haA hK hα hγ hq hψ hB] change (∫ p, (∫ ω, collisionKernel p.2.1 p.2.2 ω*f (p,ω) ∂sphereArea) ∂(coldCylinderVolume a A R ⊗ₘ E.mixedKernel ha hK hα hγ)) = _ rw [Measure.integral_compProd hF] apply integral_congr_ae filter_upwards [(Measure.integrable_compProd_iff hF.aestronglyMeasurable).mp hF |>.1] with x hx let _ : IsFiniteMeasure (E.background (max a x.1) x.2) := GeometricBackground.background_finite E.phase η E.fraction K α γ (max a x.1) x.2 rw [E.mixedKernel_apply] at hx ⊢ rw [integral_prod_symm _ hx,E.hotKernel_integral] rfl end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence end end end OAI