Parameterization of Fuel-Optimal Synchronous Approach Trajectories to Tumbling Targets
Docking with potentially tumbling Targets is a common element of many mission architectures, including on-orbit servicing and active debris removal. This paper studies synchronized docking trajectories as a way to ensure the Chaser satellite remains on the docking axis of the tumbl...
Main Authors: | Sternberg, David C., Miller, David W |
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Other Authors: | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics |
Format: | Article |
Language: | English |
Published: |
Frontiers Media SA
2020
|
Online Access: | https://hdl.handle.net/1721.1/126334 |
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