Abstract

The nonlinear adaptive attitude control problem is considered with the focus on the identification of unknown system parameters. The unknown parameters are assumed to be constant and the quaternion representation of the kinematic equations is adopted to avoid the singularity in three-parameter representations. In addition to the global asymptotic convergence of the tracking error to zero, the parameter identification is guaranteed with a simple reference signal. The parameter identification procedures rely on the shaping of the invariant manifold introduced in the adaptation algorithm. The main contribution of the paper is to propose the algorithm to identify the unknown system parameters without designing reference signals for the satisfaction of a rank condition. In order to guarantee the convergence of the estimator to the true system parameters, a three-stage estimation algorithm is proposed. At each stage, the system has a different invariant manifold in its closed-loop system dynamics. Numerical simulations demonstrate the effectiveness of the proposed method.

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call

Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.