Onboard Semianalytic Approach to Collision-Free Formation Reconfiguration


Allowing satellite formations the flexibility to perform path coming up with operations onboard each spacecraft will considerably reduce the ground operations burden and increase the responsiveness of the formation to reconfiguration events. This paper develops a semianalytic approach to fast onboard, fuel-minimized, collision-free path generation for satellites in an exceedingly formation. A sequential optimization approach to collision avoidance is examined. Through hardware testing and comparison with alternative approaches, this analytic technique shows viability for onboard, fuel-minimized, collision-free path generation.

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