Paper Citation Record · LEDGER

Saturation-Aware Robust Trajectory Optimization for Reusable Launch Vehicles via Differentiable Physics

As of 11 August 2026, this Paper Citation Record lists 21 of 21 outbound references and 0 inbound Pith citation observations for arXiv:2607.09736.

A citation records a reference. It does not transfer a finding from one paper to another.

pith.paper-citation-record.v1
2607.09736 v1

Coverage vector

measured 21 of 21 reference resolution

Typed states for the displayed outbound observations.

Source: paper_references, paper_reference_links, observed 2026-07-14T16:41:41.285102Z

measured 21 of 21 standing notices

One-hop event checks from named stored sources.

Source: scholarly_work_events, retraction_status_cache, observed 2026-08-10T06:31:04.303077+00:00

measured 0 of 0 inbound itemization

Pith citing papers itemized under the disclosed page cap.

Source: paper_references, paper_reference_links

measured 0 of 1 external citation measurements

A source-named dated measurement, never combined with another source.

Source: cited_works

Reference resolution

21 of 21 outbound references displayed

verified exact2
verified fuzzy0
unresolved19
parse uncertain0
malformed identifier0
metadata mismatch0

External citation measurements

No source-named external measurement is stored.

Outbound references

Observation 4e269c0a-02bb-4a73-8f80-4e482f223443 · outbound

This paper cites Blackmore, Autonomous precision landing of space rockets, The Bridge 46 (4) (2016) 15–20.

Saturation-Aware Robust Trajectory Optimization for Reusable Launch Vehicles via Differentiable Physics Blackmore, Autonomous precision landing of space rockets, The Bridge 46 (4) (2016) 15–20

Reference 1

Resolution: unresolved; no resolver link, observed 2026-07-14T16:41:41.285102Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

Observation 3b7b936c-ce7f-4762-9a71-568e17c9ef0a · outbound

This paper cites Lu, Propellant-optimal powered descent guidance, Journal of Guidance, Control, and Dynamics 41 (4) (2018) 813–826.

Saturation-Aware Robust Trajectory Optimization for Reusable Launch Vehicles via Differentiable Physics Lu, Propellant-optimal powered descent guidance, Journal of Guidance, Control, and Dynamics 41 (4) (2018) 813–826

Reference 2

Resolution: unresolved; no resolver link, observed 2026-07-14T16:41:41.285102Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

Observation 4070ccc1-cc9c-4fa2-a76c-9c7f0c3b43d7 · outbound

This paper cites an unresolved cited work.

Saturation-Aware Robust Trajectory Optimization for Reusable Launch Vehicles via Differentiable Physics Unresolved cited work

Reference 3

Resolution: unresolved; no resolver link, observed 2026-07-14T16:41:41.285102Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

Observation 40a901e1-ce4b-42c0-8800-94d3d651a61f · outbound

This paper cites Malyuta, et al., Advances in trajectory optimization for space vehicle control, Annual Reviews in Control 53 (2022) 130–150.

Saturation-Aware Robust Trajectory Optimization for Reusable Launch Vehicles via Differentiable Physics Malyuta, et al., Advances in trajectory optimization for space vehicle control, Annual Reviews in Control 53 (2022) 130–150

Reference 4

Resolution: unresolved; no resolver link, observed 2026-07-14T16:41:41.285102Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

Observation 273e523b-3119-42d5-923f-2e3ad3efe87b · outbound

This paper cites Acikmese, S.

Saturation-Aware Robust Trajectory Optimization for Reusable Launch Vehicles via Differentiable Physics Acikmese, S

Reference 5

Resolution: unresolved; no resolver link, observed 2026-07-14T16:41:41.285102Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

Observation 22a66d7e-1d8e-4a24-b8f5-696333f81112 · outbound

This paper cites an unresolved cited work.

Saturation-Aware Robust Trajectory Optimization for Reusable Launch Vehicles via Differentiable Physics Unresolved cited work

Reference 6

Resolution: unresolved; no resolver link, observed 2026-07-14T16:41:41.285102Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

Observation 02b4463e-08a7-4943-9c97-7a6fae918fca · outbound

This paper cites an unresolved cited work.

Saturation-Aware Robust Trajectory Optimization for Reusable Launch Vehicles via Differentiable Physics Unresolved cited work

Reference 7

Resolution: unresolved; no resolver link, observed 2026-07-14T16:41:41.285102Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

Observation a52b3ff6-681d-49be-a15c-f72c5c2e931b · outbound

This paper cites an unresolved cited work.

Saturation-Aware Robust Trajectory Optimization for Reusable Launch Vehicles via Differentiable Physics Unresolved cited work

Reference 8

Resolution: unresolved; no resolver link, observed 2026-07-14T16:41:41.285102Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

Observation 8142ebc7-cd20-4fc9-a1fb-a0cd6b61fef4 · outbound

This paper cites Okamoto, P.

Saturation-Aware Robust Trajectory Optimization for Reusable Launch Vehicles via Differentiable Physics Okamoto, P

Reference 9

Resolution: unresolved; no resolver link, observed 2026-07-14T16:41:41.285102Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

Observation 0cadd25c-1d1b-4ff4-88f5-18be85832b87 · outbound

This paper cites an unresolved cited work.

Saturation-Aware Robust Trajectory Optimization for Reusable Launch Vehicles via Differentiable Physics Unresolved cited work

Reference 10

Resolution: unresolved; no resolver link, observed 2026-07-14T16:41:41.285102Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

Observation bc3c57d6-c2b7-4137-8f23-b94a8f4ae8ec · outbound

This paper cites Mesbah, Stochastic model predictive control: An overview and perspec- tives for future research, IEEE Control Systems Magazine 36 (6) (2016) 30–44.

Saturation-Aware Robust Trajectory Optimization for Reusable Launch Vehicles via Differentiable Physics Mesbah, Stochastic model predictive control: An overview and perspec- tives for future research, IEEE Control Systems Magazine 36 (6) (2016) 30–44

Reference 11

Resolution: unresolved; no resolver link, observed 2026-07-14T16:41:41.285102Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

Observation f0b4fbe0-e37c-4d5a-987e-42205ac740c4 · outbound

This paper cites Korda, C.

Saturation-Aware Robust Trajectory Optimization for Reusable Launch Vehicles via Differentiable Physics Korda, C

Reference 12

Resolution: unresolved; no resolver link, observed 2026-07-14T16:41:41.285102Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

Observation 5ba65a53-7f18-4817-9379-56c449baf481 · outbound

This paper cites an unresolved cited work.

Saturation-Aware Robust Trajectory Optimization for Reusable Launch Vehicles via Differentiable Physics Unresolved cited work

Reference 13

Resolution: unresolved; no resolver link, observed 2026-07-14T16:41:41.285102Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

Observation 3958c108-4055-4e12-85a4-0fba7222937e · outbound

This paper cites Tarbouriech, G.

Saturation-Aware Robust Trajectory Optimization for Reusable Launch Vehicles via Differentiable Physics Tarbouriech, G

Reference 14

Resolution: verified exact; doi, observed 2026-07-14T16:50:38.334126Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-10T06:31:04.303077+00:00.

Observation fb6e4566-f713-4d91-ba97-a07bb3042a54 · outbound

This paper cites an unresolved cited work.

Saturation-Aware Robust Trajectory Optimization for Reusable Launch Vehicles via Differentiable Physics Unresolved cited work

Reference 15

Resolution: verified exact; doi, observed 2026-07-14T16:50:38.339508Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-10T06:31:04.303077+00:00.

Observation 75351c52-6cf4-471d-9111-04cacf89d606 · outbound

This paper cites Optimization of Flip-Landing Trajectories for Starship based on a Deep Learned Simulator.

Saturation-Aware Robust Trajectory Optimization for Reusable Launch Vehicles via Differentiable Physics Optimization of Flip-Landing Trajectories for Starship based on a Deep Learned Simulator

Reference 16

Resolution: unresolved; no resolver link, observed 2026-07-14T16:41:41.285102Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

Observation 3b3566d3-020c-4153-aacf-1371373435f9 · outbound

This paper cites Lipman, R.

Saturation-Aware Robust Trajectory Optimization for Reusable Launch Vehicles via Differentiable Physics Lipman, R

Reference 17

Resolution: unresolved; no resolver link, observed 2026-07-14T16:41:41.285102Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

Observation 0df32196-b7bc-4c7e-a9ba-2e58854b0acb · outbound

This paper cites Appendix A.

Saturation-Aware Robust Trajectory Optimization for Reusable Launch Vehicles via Differentiable Physics Appendix A

Reference 18

Resolution: unresolved; no resolver link, observed 2026-07-14T16:41:41.285102Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

Observation a9ec3010-1b20-45c5-9cc1-b92009869f44 · outbound

This paper cites an unresolved cited work.

Saturation-Aware Robust Trajectory Optimization for Reusable Launch Vehicles via Differentiable Physics Unresolved cited work

Reference 19

Resolution: unresolved; no resolver link, observed 2026-07-14T16:41:41.285102Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

Observation c462a679-ff16-41c4-bc4b-38d2eb839231 · outbound

This paper cites The optimization initializes with a 35 learning rate of5×10 −3 and employs aReduceLROnPlateauscheduler (decay factor =0.5, patience =150).

Saturation-Aware Robust Trajectory Optimization for Reusable Launch Vehicles via Differentiable Physics The optimization initializes with a 35 learning rate of5×10 −3 and employs aReduceLROnPlateauscheduler (decay factor =0.5, patience =150)

Reference 20

Resolution: unresolved; no resolver link, observed 2026-07-14T16:41:41.285102Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

Observation 605ced9d-388e-41af-a25e-af349ff31542 · outbound

This paper cites This theoretical margin targets an approximate99.7%constraint satisfaction probability under the local Gaussian linear propagation assumption.

Saturation-Aware Robust Trajectory Optimization for Reusable Launch Vehicles via Differentiable Physics This theoretical margin targets an approximate99.7%constraint satisfaction probability under the local Gaussian linear propagation assumption

Reference 21

Resolution: unresolved; no resolver link, observed 2026-07-14T16:41:41.285102Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

Pith citing papers

No inbound Pith citation observations are available.