论文部分内容阅读
基于最优控制理论对威胁规避约束下战斗机引导控制方法进行研究.以空战态势参数为状态建立战斗机引导模型,以引导的快速性和经济性为性能指标,将战斗机引导问题建模为具有非线性状态约束和路径约束的最优控制问题,以武器攻击包线来描述目标火力威胁,并将威胁规避约束转化为引导过程的空战态势约束问题,为保证引导算法的实时性和有效性,引入滚动时域控制策略进行在线优化,并采用高斯伪谱法进行数值求解,基于典型作战场景进行仿真,结果表明所提出的引导控制方法能在保证引导安全性的前提下实现战斗机的最优引导.
Based on the theory of optimal control, the fighter piloted control method under threat avoidance is studied.The fighter pilot model is established based on the air combat situation parameters, and the fighter piloting problem is modeled as nonlinear with the guidance of rapidity and economy as the performance index State Constraints and Path Constraints, a weapon attack envelope is used to describe the target fire threat, and the threat avoidance constraint is transformed into the air combat situation constraint problem that guides the process. To ensure the real-time performance and effectiveness of the guidance algorithm, a rolling The time domain control strategy is optimized online. The Gaussian pseudospectral method is used to solve the problem numerically. The simulation results show that the proposed guidance control method can achieve the optimal guidance of the fighter under the premise of guiding safety.