Title :
Vehicle attitude control using finite time convergence incremental nonlinear dynamic inversion combined the command differential signals
Author :
Zikang Su ; Honglun Wang ; Xingling Shao
Author_Institution :
Sch. of Autom. Sci. & Electr. Eng., Beihang Univ., Beijing, China
Abstract :
This paper presents a finite time convergence incremental nonlinear dynamic inversion combined the command differential signals feed forward control. It shows better performance in handling command signals´ tracking problems caused by the time delay of angular acceleration feedback signals´ acquisition in regular incremental nonlinear dynamic inversion, with the combination of finite time convergence desired outputs and command differential signals. The status tracking error convergence theorem for finite time convergence incremental nonlinear dynamic inversion is proved, together with model mismatch perturbation analysis. Simulation results demonstrate, the method presented in this paper not only shows insensitive to model mismatch as the regular incremental nonlinear dynamic inversion, but also tracks the command signal without error in real time.
Keywords :
aircraft control; attitude control; delays; feedforward; nonlinear dynamical systems; signal detection; angular acceleration feedback signal acquisition; command differential signal feedforward control; command signal tracking problems; finite time convergence incremental nonlinear dynamic inversion; model mismatch perturbation analysis; regular incremental nonlinear dynamic inversion; status tracking error convergence theorem; time delay; vehicle attitude control; Acceleration; Actuators; Attitude control; Convergence; Delay effects; Nonlinear dynamical systems; Vectors;
Conference_Titel :
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location :
Yantai
Print_ISBN :
978-1-4799-4700-3
DOI :
10.1109/CGNCC.2014.7007355