Title :
Attitude stabilization with actuators subject to switching-time constraints using explicit MPC
Author :
Vieira, Márcio Santos ; Galvão, Roberto Kawakami Harrop ; Kienitz, Karl Heinz
Author_Institution :
Dept. de Sist. e Controle, Inst. Tecnol. de Aeronaut., Sao Paulo, Brazil
Abstract :
This paper is concerned with the design of an explicit model predictive controller (eMPC) for attitude stabilization using on-off thrusters subject to switching-time constraints. 12In the proposed approach, the control actions are specified by a sequence of integer values in the set {-1, 0, +1}, i.e the thrusters can be fully opened in one of two possible directions (-1 or +1) or remain closed (0). Switching-time constraints are taken into account by imposing restrictions on the minimum number of consecutive equal elements in the control sequence. The explicit solution to the constrained MPC problem is computed by solving a multi-parametric mixed integer linear program (mpMILP), where the parameters are the components of the state vector. The solution to the mpMILP is a piecewise affine (PWA) function, which can be evaluated at each sampling time to obtain the optimal control law. Since the on-line computation effort is restricted to a table-lookup, the controller can be implemented using a simple computational hardware.
Keywords :
actuators; attitude control; control system synthesis; integer programming; linear programming; predictive control; stability; table lookup; time-varying systems; attitude stabilization; computational hardware; constrained MPC problem; integer value; model predictive controller; multiparametric mixed integer linear program; on-line computation effort; on-off thruster; optimal control law; piecewise affine function; switching time constraint; table lookup; Actuators; Attitude control; Optimal control; Optimization; Predictive models; Switches;
Conference_Titel :
Aerospace Conference, 2011 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4244-7350-2
DOI :
10.1109/AERO.2011.5747482