PD adaptive controller method for a three-axis stabilized rigid satellite attitude system
نویسندگان
چکیده
This paper deals with the attitude tracking control problem of rigid satellite uncertainties disturbances. An adaptive proportional derivative controller (PD) is proposed to deal influence external disturbance in controller. The uncertain disturbances can be estimated through an algorithm and compensated error closed-loop system stability are ensured based on Lyapunov analysis. using representation spacecraft dynamics especially quaternion properties.Simulation results clearly illustrate feasibility, effectiveness performance planned strategies, which have been validated by Monte Carlo method, extended other laws.
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ژورنال
عنوان ژورنال: Algerian journal of signals and systems
سال: 2023
ISSN: ['2676-1548', '2543-3792']
DOI: https://doi.org/10.51485/ajss.v8i1.181