Yuan Zihuai. AN APPROXIMATE METHOD OF DECOUPLING LONGITUDINAL AND LATERAL MOTIONS OF ROLLING MISSILESJ. Transactions of Beijing institute of Technology, 1989, (2): 41-50.
Citation:
Yuan Zihuai. AN APPROXIMATE METHOD OF DECOUPLING LONGITUDINAL AND LATERAL MOTIONS OF ROLLING MISSILESJ. Transactions of Beijing institute of Technology, 1989, (2): 41-50.
Yuan Zihuai. AN APPROXIMATE METHOD OF DECOUPLING LONGITUDINAL AND LATERAL MOTIONS OF ROLLING MISSILESJ. Transactions of Beijing institute of Technology, 1989, (2): 41-50.
Citation:
Yuan Zihuai. AN APPROXIMATE METHOD OF DECOUPLING LONGITUDINAL AND LATERAL MOTIONS OF ROLLING MISSILESJ. Transactions of Beijing institute of Technology, 1989, (2): 41-50.
AN APPROXIMATE METHOD OF DECOUPLING LONGITUDINAL AND LATERAL MOTIONS OF ROLLING MISSILES
A method for decoupling the longitudinal and lateral motions of rolling missiles is presented in this paper, in order to realize an average decoupling of the guided missile motions along the whole trajectory,a compensation angle can be set using a three-degree-of-freedom gyro. In addition, design parameters are optimized by Powell's method.
DownLoad: