摘要
给出了航路飞行自动飞行仿真的总体框架,介绍了采用分段线性函数描述控制指令的机动指令生成器算法,对机动指令跟踪器的控制律结构进行了设计,并对其参数进行了整定与调整。采用飞机六自由度模型对航路飞行过程进行了自动飞行仿真。仿真结果表明,飞机能够较好地完成航路飞行仿真任务。
The automatic flight simulation of waypoint flight was conducted using the 6 degree-of-freedom aircraft model. The automatic flight simulation system framework of waypoint flight was presented. The algorithm of the maneuvering command generator was introduced, which using the subsection linearity function method. The control structure of the maneuvering command tracker was designed, and the parameters were scheduled. The simulation results show that the waypoint flight can be well accomplished.
出处
《飞行力学》
CSCD
北大核心
2008年第1期75-78,共4页
Flight Dynamics
关键词
航路飞行
自动飞行仿真
机动指令生成器
机动指令跟踪器
waypoint flight
automatic flight simulation
maneuvering command generator
maneuvering command tracker
