Model-Free Attitude Control of Spacecraft Based on PID-Guide TD3 Algorithm
نویسندگان
چکیده
منابع مشابه
Pid+ Backstepping Control of Relative Spacecraft Attitude
In this paper we present a PID+ backstepping controller, as a solution to the problem of coordinated attitude control in spacecraft formations. The control scheme is based on quaternions and modified Rodriguez parameters as attitude representation of the relative attitude error. Utilizing the invertibility of the modified Rodriguez parameter kinematic differential equation, a globally exponenti...
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ژورنال
عنوان ژورنال: International Journal of Aerospace Engineering
سال: 2020
ISSN: 1687-5974,1687-5966
DOI: 10.1155/2020/8874619