Symmetry properties of optimal relative orbit trajectories
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Publication:1665243
DOI10.1155/2015/286525zbMath1394.70059OpenAlexW1539925055WikidataQ59117866 ScholiaQ59117866MaRDI QIDQ1665243
Publication date: 27 August 2018
Published in: Mathematical Problems in Engineering (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1155/2015/286525
Cites Work
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- Optimal low-thrust orbital maneuvers via indirect swarming method
- General theory of optimal trajectory for rocket flight in a resisting medium
- Fuel-optimal maneuvers of a spacecraft relative to a point in circular orbit
- State Transition Matrices for Terminal Rendezvous Studies: Brief Survey and New Example
- An intelligent control concept for formation flying satellites
- Optimal four-impulse fixed-time rendezvous in the vicinity of a circular orbit.
- Optimal two- and three-impulse fixed-time rendezvous in the vicinityof a circular orbit
- \(J_2\) invariant relative orbits for spacecraft formations
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