Air Vehicles Attitude Control System Based on Virtual Instrument
As an important part of the air vehicles control systems, the attitude control system has an important effect to the vehicles performance. This paper introduces a new method of development of the Vehicles Attitude Control System by using Virtual Instrument. In the system, the air vehicles attitude signals which come from SINS on two-axis turntable are received by RS232 in real-time, at the same time Control Algorithm in computer give the output Control signals to Actuator via NI-DAQ. Air vehicle model and theoretic trajectory are given by MATLAB/Simulink which can be carried out in LabVIEW. By using technology of Virtual Instrument, the parameters of the Air Vehicle can be show timely, Control Algorithm can be improved in real-time, and the performance of the Control Actuator can be tested all through. This system has hardware-in-loop which strengthens the reliability and authenticity.
Attitude Control System Virtual Instrument MATLAB/Simulink
Zhang Weina Su Zhong Xia Yan Xu Dawei
Beijing Information Technology Institute Beijing 100101 China
国际会议
西安
英文
2007-08-16（万方平台首次上网日期，不代表论文的发表时间）