Affiliation:
1. Key Laboratory of Dynamic and Control of Flight Vehicle, Ministry of Education, Beijing Institute of Technology, Beijing, China
Abstract
The maximum down range trajectory optimization problem with multiple phases and multiple constraints corresponding to the flight of a boost-glide vehicle is considered. The longitudinal motion model was built as a multiphase optimization problem under constraints. Legendre–Gauss–Radau collocation points were used to transcribe the optimization problem into a finite-dimensional nonlinear programming problem, and the maximization down range trajectory was obtained based on adaptive mesh refinement pseudospectral methods. However, sometimes it is difficult to find interior points without position constraints. A novel optimization strategy based on dynamic programming theory was proposed to search the free interior points more accurately and quickly, which resulted in almost the same optimized trajectory while producing a small mesh. The results of numerical examples showed that the boost-glide vehicle trajectory optimization problem is solved using the adaptive mesh refinement pseudospectral methods.
Subject
Mechanical Engineering,Aerospace Engineering
Cited by
5 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Fluid Simulation of Trajectory Stabilization System for High Speed Aircraft;2022 5th World Conference on Mechanical Engineering and Intelligent Manufacturing (WCMEIM);2022-11-18
2. Trajectory Optimization of a Subsonic Unpowered Gliding Vehicle Using Control Vector Parameterization;Drones;2022-11-17
3. A modified pseudospectral method for indirect solving a class of switching optimal control problems;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2020-04-03
4. Conceptual study of a dual-rocket-based-combined-cycle powered two-stage-to-orbit launch vehicle;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2017-05-01
5. Atmospheric vehicle trajectory optimization with minimum dynamic pressure constraint;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2017-04-30