多体卫星高稳定度智能控制方案研究  

Intelligent Control Research of Multibody Satellite for High Stability

作　　者：李广兴[1] 周军[1] 周凤岐[1] 

机构地区：[1]西北工业大学航天学院,西安710072

出　　处：《空间科学学报》2007年第2期151-156,共6页Chinese Journal of Space Science

摘　　要：卫星上大型挠性天线的加减速运动会对星体产生较大的扰动,影响了星体姿态的指向精度和稳定度．运用Lyapunov稳定性理论,设计了变结构和神经网络控制器,并在星体前馈中引入扰动补偿力矩,从而保证星体姿态角速度在不确定性干扰下能以指数形式收敛到某一给定的有界范围内,仿真证明了姿态的稳定度满足给定的指标要求．Control system of multibody satellite is designed to improve attitude stability in this paper. The control law consisting of variable structure control and neural network control is obtained by using Lyapunov stability theory. Variable structure control is a nonlinear control strategy employing feedback of a discontinuous signal, and is very robust to matched plant uncertainties and external disturbances when state variables enter the sliding surface. Neural network systems are physical cellular systems that can acquire, store, and utilize experiential knowledge. The knowledge is in the form of stable states or mappings embedded in networks that can be recalled in response to the presentation of the data input to the network systems. The application of the neural network is made possible by recognizing function approximation capability in this paper. Since dynamics of multibody satellite can not be obtained accurately, the conventional controllers will not ensure the good performance of control system. A suitable technique cope with such system is variable structure control and neural network control. By Integrating their merits, robust capability and high control accuracy can be achieved. In addition, compensation control is introduced into the feedforward loop to eliminate the disturbance caused by the motion of antenna, so convergence of angular velocity is in the form of exponent guaranteed. Simulation results illustrate the control system has the good attitude stable characteristics using the proposed controller in the presence of external disturbances and parameters uncertainties.

关 键 词：挠性天线 变结构控制 神经网络 自适应控制 

分 类 号：V448.2[航空宇航科学与技术—飞行器设计]