论文部分内容阅读
针对多操纵面飞行器的控制分配问题,提出了一种基于BFGS算法的控制分配策略。该分配策略克服了不动点迭代算法分配时舵面容易饱和的缺点。为验证BFGS分配策略的可行性和有效性,以某型战斗机为研究对象,进行了控制分配和重构仿真。仿真结果表明,该分配策略能将飞行指令在舵面饱和范围内合理地分配在各个舵面上。
Aiming at the control assignment of multi-control plane aircraft, a control strategy based on BFGS algorithm is proposed. The distribution strategy overcomes the shortcomings that the fixed rudder surface is easy to be saturated when the fixed point iteration algorithm is distributed. In order to verify the feasibility and effectiveness of the BFGS allocation strategy, a certain type of fighter aircraft was selected as the research object and the control distribution and reconstruction simulation were carried out. The simulation results show that the distribution strategy can distribute the flight commands to all the control surfaces within the saturation range of the control surface.