计算机应用与软件2024，Vol.41Issue(6)：134-141,193,9.DOI:10.3969/j.issn.1000-386x.2024.06.020
基于改进hp自适应RPM的客机最速爬升轨迹优化
THE FAST CLIMB TRAJECTORY OPTIMIZATION OF AIRCRAFT BASED ON IMPROVED HP ADAPTIVE RPM
吴凯1
作者信息
- 1. 北京飞机维修工程有限公司西南航线中心一大队一中队 四川成都 610200
- 折叠
摘要
Abstract
Aimed at the optimization problem of the fastest time climb of the passenger aircraft,the improved hp adaptive Radau pseudospectral method(RPM)is used to discretize the continuous-time optimal control of passenger aircraft climb into a nonlinear programming problem to solve.The experimental simulation results verify that the optimized aircraft climbing trajectory can complete the fastest time climbing under the premise of meeting the performance constraints of the passenger aircraft and the passenger experience,and achieve cruise altitude and cruising speed.Compared with the hp adaptive Radau pseudospectral method,the improved method can complete the optimization process with higher solving efficiency on the basis of ensuring the optimality of the optimization solution.关键词
民航飞机/轨迹优化/伪谱法Key words
Aircraft/Trajectory optimization/Pseudospectral method分类
信息技术与安全科学引用本文复制引用
吴凯..基于改进hp自适应RPM的客机最速爬升轨迹优化[J].计算机应用与软件,2024,41(6):134-141,193,9.
