论文信息 - Real time hardware-in-loop simulation of ESMO satellite attitude control system

Real time hardware-in-loop simulation of ESMO satellite attitude control system

This paper studies attitude control of the ESMO satellite using six reaction thrusters. Bang-bang control with dead-zone and Pulse-Width Modulation (PWM) for the modulation of the on-time of the thrusters are treated. Closed loop hardware-in-loop simulations, using the microcontroller unit (MCU) Microchip PIC18F452 for implementation of attitude control and MatLab in a standard PC for simulating satellite dynamics, are carried out. Results for real time simulation are compared with autonomous simulations. The controller gives a satisfactory performance in the real time environment.

[1] Audra E. Kosh,et al. Linear Algebra and its Applications , 1992 .

[2] P. Y. Willems,et al. SPACECRAFT DYNAMICS AND CONTROL , 1981 .

[3] Christopher D. Hall,et al. Spacecraft Dynamics and Control , 2002 .

[4] Jan Tommy Gravdahl,et al. Modeling and simulation for automatic control , 2002 .

[5] Willem H. Steyn,et al. In-Orbit Estimation of the Inertia Matrix and Thruster Parameters of UoSAT-12 , 2000 .

[6] Ling Hou,et al. Stability analysis of pulsewidth-modulated feedback systems , 2000, Proceedings of the 39th IEEE Conference on Decision and Control (Cat. No.00CH37187).