Adaptive Reduced Attitude Control for Rigid Spacecraft With Elliptical Pointing Constraints

Yueyang Liu, Qinglei Hu, Gang Feng 0001. Adaptive Reduced Attitude Control for Rigid Spacecraft With Elliptical Pointing Constraints. IEEE Trans. Aerospace and Electronic Systems, 59(4):3835-3847, August 2023. [doi]

Abstract

Abstract is missing.