Affiliation:
1. School of Astronautics, Harbin Institute of Technology, China
2. Key Laboratory of System Control and Information Processing, Ministry of Education, China
Abstract
In order to deal with the problem of attitude tracking control for quadrotors subject to time-varying inertia and external disturbances, a finite-time bounded switched linear parameter-varying (LPV) control method is presented. The attitude dynamics is described by two subsystems, where the inner angular-velocity system is used to track the desired angular velocities that are generated by the outer attitude-angle system. The angular-velocity system of quadrotors is modeled as a switched LPV model, where a family of linear models is developed to approximate the original nonlinear system and the LPV method is applied to model the time-varying inertia. Specially, a mode-dependent persistent dwell-time (MPDT) switching logic, which is more general than the typically used dwell-time (DT) or average dwell-time (ADT) switching logic, is adopted to govern the switching behaviors among these linear models. A state-feedback controller for the switched LPV error-tracking system is designed, which ensures both finite-time boundedness and extended dissipative performance. Finally, the developed theoretical results are verified by numerical simulation.
Funder
State Administration of Science, Technology and Industry for National Defense
Heilongjiang Provincial Postdoctoral Science Foundation
China Postdoctoral Science Foundation
National Natural Science Foundation of China
Key Laboratory of Ministry of Education of System Control and Information Processing
Natural Science Foundation of Heilongjiang Province, China
Cited by
5 articles.
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