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eess.SY2026
Two-impulse Rendezvous Planning about Thrusting Spacecraft on SE2(3)
Micah Condie, Abigaile Woodbury, James Goppert
The classical Hill--Clohessy--Wiltshire equations assume an unforced Keplerian reference trajectory, an assumption that is violated by missions requiring continuous thrust. We form…
eess.SY2025
Log-linear Dynamic Inversion for Thrusting Spacecraft on SE2(3)
Micah K. Condie, Abigaile E. Woodbury, Li-Yu Lin +3
Body-fixed spacecraft thrust couples attitude tracking error to translational motion because the applied inertial acceleration depends on spacecraft attitude. In this work, we form…