Attitude tracking control of rigid spacecraft with disturbance compensation
نویسندگان
چکیده
منابع مشابه
Smooth Adaptive Finite Time Attitude Tracking Control of Rigid Spacecraft
This paper investigates two chattering-free finite-time controllers for the rigid spacecraft attitude tracking control problem considering modeling uncertainty and external disturbance. First, the basic controller is designed utilizing integral terminal sliding mode surface (ITSMS) with prior knowledge of the total system uncertainty consisting of modeling uncertainty and external disturbance. ...
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ژورنال
عنوان ژورنال: International Journal of Modelling, Identification and Control
سال: 2019
ISSN: 1746-6172,1746-6180
DOI: 10.1504/ijmic.2019.10017462