Title :
Direction-cosine-matrix-based attitude control subject to actuator saturation
Author :
Forbes, James Richard
Author_Institution :
Dept. of Aerosp. Eng., Univ. of Michigan, Ann Arbor, MI, USA
Abstract :
Set-point attitude control of a rigid body explicitly preventing actuator saturation is considered. The attitude control approach developed does not employ any sort of direction-cosine-matrix (DCM) parameterisation, such as Euler angles or quaternions. Rather, the DCM is used directly within the feedback control algorithm. Together a proportional control term and an angular velocity control term make up the attitude controller. The angular velocity control is composed of a strictly positive real system subject to a special input non-linearity. The specific form of the proportional control and angular velocity control ensure control torques are below the saturation level of the on-board actuators. Two controller synthesis methods are considered. The first uses the linearised system, the solution to the linear quadratic regulator problem, and the Kalman-Yakubovich-Popov lemma to design the controller. The second employs a simple low-pass filter that is guaranteed to stabilise the closed-loop system; tuning the low-pass filter is also considered. Numerical simulation results demonstrate effective closed-loop control in the presence of plant disturbances and sensor noise.
Keywords :
aerospace robotics; angular velocity control; attitude control; closed loop systems; control nonlinearities; control system synthesis; feedback; linear quadratic control; linearisation techniques; low-pass filters; matrix algebra; DCM; Euler angles; Kalman-Yakubovich-Popov lemma; actuator saturation; angular velocity control term; closed-loop system; controller synthesis methods; direction-cosine-matrix parameterisation; direction-cosine-matrix-based attitude control; feedback control algorithm; input nonlinearity; linear quadratic regulator problem; linearised system; low-pass filter; on-board actuators; plant disturbances; proportional control; quaternions; rigid body; sensor noise; set-point attitude control;
Journal_Title :
Control Theory & Applications, IET
DOI :
10.1049/iet-cta.2014.0890