Dual Channel Maneuver Flight Control Based on Dynamic Inverse and Dynamic Sliding Mode

Authors

Shengyi Yang, 1.Key Laboratory of Pattern Recognition and Intelligent Systems of Guizhou Province, Guizhou Minzu University, Guiyang 550025, China; ;2.Key Laboratory of Dynamics and Control of Flight Vehicle , Ministry of Education , Beijing Institute of Technology, Beijing 100081, China;
Liu Chao, 2.Key Laboratory of Dynamics and Control of Flight Vehicle , Ministry of Education , Beijing Institute of Technology, Beijing 100081, China;
Shengjing Tang, 2.Key Laboratory of Dynamics and Control of Flight Vehicle , Ministry of Education , Beijing Institute of Technology, Beijing 100081, China;
Weili Yang, 1.Key Laboratory of Pattern Recognition and Intelligent Systems of Guizhou Province, Guizhou Minzu University, Guiyang 550025, China; ;

Abstract

Abstract: In order to solve the flight control problem of mini quadrotor with large angle and fast maneuver, a new dual channel maneuver flight control method based on dynamic inverse (DI) and sliding mode control (SMC) is proposed. By combining SMC and DI, this method makes the system robust to the model uncertainty and aerodynamic interference. The dynamic SMC effectively reduces system’s chattering. New sliding mode surface and quaternion regular model of aircraft attitude are built to improve the control precision and resolve the singular problem of aircraft. The DI improves the system’s dynamic response, and the stability analysis of zero dynamics is given in the inverse system design. The simulation results show the effectiveness of the proposed control scheme.

Recommended Citation

Yang, Shengyi; Chao, Liu; Tang, Shengjing; and Yang, Weili (2019) "Dual Channel Maneuver Flight Control Based on Dynamic Inverse and Dynamic Sliding Mode," Journal of System Simulation: Vol. 30: Iss. 1, Article 19.
DOI: 10.16182/j.issn1004731x.joss.201801019
Available at: https://dc-china-simulation.researchcommons.org/journal/vol30/iss1/19

First Page

156

DOI Link

https://doi.org/10.16182/j.issn1004731x.joss.201801019

Last Page

164

CLC

V249.12

Recommended Citation

Yang Shengyi, Liu Chao, Tang Shengjing, Yang Weili. Dual Channel Maneuver Flight Control Based on Dynamic Inverse and Dynamic Sliding Mode[J]. Journal of System Simulation, 2018, 30(1): 156-164.

DOI

10.16182/j.issn1004731x.joss.201801019