Paper Citation Record · LEDGER

Mass-Optimal Low-Thrust Forced Periodic Trajectories in the Earth-Moon CR3BP

As of 22 August 2026, this Paper Citation Record lists 20 of 20 outbound references and 0 inbound Pith citation observations for arXiv:2502.05140.

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

pith.paper-citation-record.v1
2502.05140 v1

Coverage vector

measured 20 of 20 reference resolution

Typed states for the displayed outbound observations.

Source: paper_references, paper_reference_links, observed 2026-08-08T20:11:56.488726Z

measured 20 of 20 standing notices

One-hop event checks from named stored sources.

Source: scholarly_work_events, retraction_status_cache, observed 2026-08-22T06:32:14.747728+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

20 of 20 outbound references displayed

verified exact9
verified fuzzy6
unresolved4
parse uncertain0
malformed identifier1
metadata mismatch0

External citation measurements

No source-named external measurement is stored.

Outbound references

Observation 5008632c-c37d-437e-bdad-b55269e4c0f1 · outbound

This paper cites Solar sail parking in restricted three-body systems,.

Mass-Optimal Low-Thrust Forced Periodic Trajectories in the Earth-Moon CR3BP Solar sail parking in restricted three-body systems,

Reference 1

Resolution: unresolved; no resolver link, observed 2026-08-08T20:11:56.428658Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

Observation 2d6fe805-f5cc-47f7-ba87-71704a54a226 · outbound

This paper cites Artificial Equilibrium Points in the Low-Thrust Re- stricted Three-Body Problem,.

Mass-Optimal Low-Thrust Forced Periodic Trajectories in the Earth-Moon CR3BP Artificial Equilibrium Points in the Low-Thrust Re- stricted Three-Body Problem,

Reference 2

Resolution: verified exact; doi, observed 2026-08-08T20:11:56.604587Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-22T06:32:14.747728+00:00.

Observation f7a87c12-221f-45c8-8fd4-a1783d1e0764 · outbound

This paper cites Artificial Three-Body Equilibria for Hybrid Low-Thrust Propulsion,.

Mass-Optimal Low-Thrust Forced Periodic Trajectories in the Earth-Moon CR3BP Artificial Three-Body Equilibria for Hybrid Low-Thrust Propulsion,

Reference 3

Resolution: verified exact; doi, observed 2026-08-08T20:11:56.594850Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-22T06:32:14.747728+00:00.

Observation c0ae462b-e8f8-48d9-bc9e-dd56afc0a9e3 · outbound

This paper cites Dynamical structures in a low-thrust, multi-body model with ap- plications to trajectory design,.

Mass-Optimal Low-Thrust Forced Periodic Trajectories in the Earth-Moon CR3BP Dynamical structures in a low-thrust, multi-body model with ap- plications to trajectory design,

Reference 4

Resolution: malformed identifier; no resolver link, observed 2026-08-08T20:11:56.439649Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

Observation 7f9c8a7e-0f75-4d30-b6ed-d167fe5b790f · outbound

This paper cites Trajectory Design Leveraging Low-Thrust, Multi-Body Equi- libria and their Manifolds,.

Mass-Optimal Low-Thrust Forced Periodic Trajectories in the Earth-Moon CR3BP Trajectory Design Leveraging Low-Thrust, Multi-Body Equi- libria and their Manifolds,

Reference 5

Resolution: verified exact; doi, observed 2026-08-08T20:11:56.579646Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-22T06:32:14.747728+00:00.

Observation e95c52e2-54f9-4c6e-878a-e9dafd2a1b5f · outbound

This paper cites Periodic Orbits with Low-Thrust Propulsion in the Re- stricted Three-body Problem,.

Mass-Optimal Low-Thrust Forced Periodic Trajectories in the Earth-Moon CR3BP Periodic Orbits with Low-Thrust Propulsion in the Re- stricted Three-body Problem,

Reference 6

Resolution: verified exact; doi, observed 2026-08-08T20:11:56.570781Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-22T06:32:14.747728+00:00.

Observation 2ed35121-b557-44e9-b31c-dfc265f70859 · outbound

This paper cites Low-Thrust Orbit Dynamics and Periodic Trajectories in the Earth–Moon System,.

Mass-Optimal Low-Thrust Forced Periodic Trajectories in the Earth-Moon CR3BP Low-Thrust Orbit Dynamics and Periodic Trajectories in the Earth–Moon System,

Reference 7

Resolution: verified exact; doi, observed 2026-08-08T20:11:56.560778Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-22T06:32:14.747728+00:00.

Observation 434ca606-3db7-49ae-9eb5-15d329375ae8 · outbound

This paper cites Artificial halo orbits for low-thrust propulsion spacecraft,.

Mass-Optimal Low-Thrust Forced Periodic Trajectories in the Earth-Moon CR3BP Artificial halo orbits for low-thrust propulsion spacecraft,

Reference 8

Resolution: verified exact; doi, observed 2026-08-08T20:11:56.551594Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-22T06:32:14.747728+00:00.

Observation f5abf7b7-d08b-4863-a706-d26ac1faa586 · outbound

This paper cites New Equilibria and Dynamic Structures Under Continuous Optimal Feedback Control,.

Mass-Optimal Low-Thrust Forced Periodic Trajectories in the Earth-Moon CR3BP New Equilibria and Dynamic Structures Under Continuous Optimal Feedback Control,

Reference 9

Resolution: unresolved; no resolver link, observed 2026-08-08T20:11:56.455549Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

Observation 6b2ff634-52e9-44ef-af91-6dce151d1f54 · outbound

This paper cites Natural and Forced Spacecraft Loitering in a Near Rectilinear Halo Orbit,.

Mass-Optimal Low-Thrust Forced Periodic Trajectories in the Earth-Moon CR3BP Natural and Forced Spacecraft Loitering in a Near Rectilinear Halo Orbit,

Reference 10

Resolution: verified exact; doi, observed 2026-08-08T20:11:56.535800Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-22T06:32:14.747728+00:00.

Observation db6d6c60-3acd-4ec5-9f3b-f24950ac7bb3 · outbound

This paper cites Generation of energy-optimal low-thrust forced periodic trajectories in the cr3bp,.

Mass-Optimal Low-Thrust Forced Periodic Trajectories in the Earth-Moon CR3BP Generation of energy-optimal low-thrust forced periodic trajectories in the cr3bp,

Reference 11

Resolution: verified fuzzy; raw_fallback, observed 2026-08-08T20:11:56.732775Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-22T06:32:14.747728+00:00.

Observation ec3a90c9-2545-4e52-a055-38e20373d45a · outbound

This paper cites an unresolved cited work.

Mass-Optimal Low-Thrust Forced Periodic Trajectories in the Earth-Moon CR3BP Unresolved cited work

Reference 12

Resolution: unresolved; no resolver link, observed 2026-08-08T20:11:56.464272Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

Observation 7528d510-e3eb-4167-970b-9c793dbf05f1 · outbound

This paper cites ASSET: Astrodynamics Software and Science Enabling Toolkit,.

Mass-Optimal Low-Thrust Forced Periodic Trajectories in the Earth-Moon CR3BP ASSET: Astrodynamics Software and Science Enabling Toolkit,

Reference 13

Resolution: verified exact; doi, observed 2026-08-08T20:11:56.526614Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-22T06:32:14.747728+00:00.

Observation 9ea9a4fd-4c49-459f-a8ca-83ca2c367d40 · outbound

This paper cites Enhancements to the Astrodynamics Software and Science Enabling Toolkit (ASSET),.

Mass-Optimal Low-Thrust Forced Periodic Trajectories in the Earth-Moon CR3BP Enhancements to the Astrodynamics Software and Science Enabling Toolkit (ASSET),

Reference 14

Resolution: verified fuzzy; raw_fallback, observed 2026-08-08T20:11:56.717767Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-22T06:32:14.747728+00:00.

Observation 36403868-7b95-4e7f-9d9e-bf6f3f1f9e3b · outbound

This paper cites Pezent, On the Implementation and Applications of a High Performance Trajectory Optimization Toolkit.

Mass-Optimal Low-Thrust Forced Periodic Trajectories in the Earth-Moon CR3BP Pezent, On the Implementation and Applications of a High Performance Trajectory Optimization Toolkit

Reference 15

Resolution: verified fuzzy; raw_fallback, observed 2026-08-08T20:11:56.708116Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-22T06:32:14.747728+00:00.

Observation eba4c5c5-109e-4ecd-82b8-8b65a074be4c · outbound

This paper cites Comparing Relative Reahcable Sets About Nearly Circular Orbits,.

Mass-Optimal Low-Thrust Forced Periodic Trajectories in the Earth-Moon CR3BP Comparing Relative Reahcable Sets About Nearly Circular Orbits,

Reference 16

Resolution: verified fuzzy; raw_fallback, observed 2026-08-08T20:11:56.698547Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-22T06:32:14.747728+00:00.

Observation da70372d-e37f-4847-8b20-641c0dd7c78d · outbound

This paper cites Reachable set computation for spacecraft relative motion with energy-limited low-thrust,.

Mass-Optimal Low-Thrust Forced Periodic Trajectories in the Earth-Moon CR3BP Reachable set computation for spacecraft relative motion with energy-limited low-thrust,

Reference 17

Resolution: verified fuzzy; raw_fallback, observed 2026-08-08T20:11:56.690158Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-22T06:32:14.747728+00:00.

Observation 0e630123-e5e6-454b-b75d-fc855d488c7f · outbound

This paper cites Analysis on reachable set for spacecraft relative motion under low-thrust,.

Mass-Optimal Low-Thrust Forced Periodic Trajectories in the Earth-Moon CR3BP Analysis on reachable set for spacecraft relative motion under low-thrust,

Reference 18

Resolution: verified fuzzy; raw_fallback, observed 2026-08-08T20:11:56.680208Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-22T06:32:14.747728+00:00.

Observation 240118a2-49b1-484c-9f08-5e4f09726407 · outbound

This paper cites Particle swarm optimization,.

Mass-Optimal Low-Thrust Forced Periodic Trajectories in the Earth-Moon CR3BP Particle swarm optimization,

Reference 19

Resolution: unresolved; no resolver link, observed 2026-08-08T20:11:56.486313Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

Observation 4c511561-2198-4468-ac27-a6686b4aac2e · outbound

This paper cites Chaos-enhanced accelerated particle swarm optimization,.

Mass-Optimal Low-Thrust Forced Periodic Trajectories in the Earth-Moon CR3BP Chaos-enhanced accelerated particle swarm optimization,

Reference 20

Resolution: verified exact; doi, observed 2026-08-08T20:11:56.517043Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-22T06:32:14.747728+00:00.

Pith citing papers

No inbound Pith citation observations are available.