OPTIMAL GUIDANCE TRAJECTORIES FOR A NANOSATELLITE DOCKING WITH A TUMBLING RESIDENT SPACE OBJECT USING A HIGH FIDELITY J2 AND QUADRATIC DRAG PERTURBATIONS MODEL
IAF Astrodynamics Symposium ; 2019 ; Washington, DC
2020
Conference paper
English
Optimal Rendezvous Trajectories of a Controlled Spacecraft and a Tumbling Object
Online Contents | 2011
|Drag coefficients for tumbling satellites.
AIAA | 1967
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