Design of a Trajectory Planning Method Oriented to Generalized Simulation

The current common design method of missile trajectory planning algorithm, for the occasions that need to simulate multiple types of missiles, has the disadvantages of a heavy workload in the processing of missile mathematical models and a narrow application range of algorithm parameters. In this paper, based on Newton’s method, a more general trajectory planning method that can adapt to various types of missiles is designed. This method is designed based on the design ideas of model black-box and multi-stage optimization, which is adaptable to various types of missiles, easy to implement in engineering, and easy to replace the type of model.