Title :
Multi-model soft switching tracking control and robust least-squares weighted control allocation for near space interceptor
Author :
Guo Chao ; Liang Xiao-Geng ; Wang Jun-Wei
Author_Institution :
Sch. of Autom., Northwestern Polytech. Univ., Xi´an, China
Abstract :
This paper deals with the multi-model soft switching tracking control (MMSSTC) design problem with a disturbance observer and a new robust least-squares weighted control allocation (RLSWCA) method for the near space interceptor (NSI) with aerodynamic fins and reaction jets. Initially, the flight envelop of the NSI is divided into some small subregions by the fuzzy partition method, a slow-fast loop soft switching model is constructed to represent the NSI system based on the local Takagi-Sugeno (T-S) model, and a disturbance observer is proposed to estimate the unknown disturbance. Then, based on the descriptor system method, a MMSSTC is developed to not only ensure the stability of the closed-loop NSI system, but also achieve a specified control performance. Furthermore, a new RLSWCA algorithm is employed to distribute the virtual control command among the redundant actuators. The purpose of this algorithm is to find the optimal control vector of the actuators by minimizing the worse-case residual, while taking into account of the uncertainty in the control effectiveness matrix and the actuator constraints. Finally, simulation results on the NSI demonstrate the effectiveness of the proposed control scheme.
Keywords :
actuators; aerodynamics; aircraft control; closed loop systems; fuzzy control; jets; least squares approximations; matrix algebra; observers; optical control; robust control; stability; time-varying systems; vectors; vehicle dynamics; MMSSTC; NSHV; RLSWCA; T-S model; actuator constraints; aerodynamic fins; closed-loop NSI system stability; control effectiveness matrix; disturbance observer; flight envelop; fuzzy partition method; local Takagi-Sugeno model; multimodel soft switching tracking control design problem; near space air-breathing hypersonic vehicles; near space interceptor; optimal control vector; reaction jets; robust least-squares weighted control allocation method; slow-fast loop soft switching model; unknown disturbance estimation; virtual control command; worse-case residual minimization; Actuators; Aerodynamics; Observers; Resource management; Soft switching; Vectors; Disturbance observer; Linear matrix inequalities (LMIs); Near space interceptor (NSI); Robust least-squares weighted control allocation (RLSWCA); Soft switching;
Conference_Titel :
Control Conference (CCC), 2014 33rd Chinese
Conference_Location :
Nanjing
DOI :
10.1109/ChiCC.2014.6895644