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考虑可变约束的轨道交会调相机动策略优化OA

Spacecraft Phasing Maneuver Strategy Optimization Considering Variable Constraints for Orbital Rendezvous Mission

中文摘要英文摘要

针对目标航天器与追踪航天器交会对接任务的调相机动规划需求,提出一种考虑可变约束的轨道交会目标航天器调相机动策略优化方法.首先,通过非线性规划问题的建模与具体约束条件的分析,将轨道预报过程产生的可变约束转化为固定约束;接着,借助微分修正(Dif-ferentialCorrection,DC)和序列二次规划(Sequential Quadratic Programming,SQP)的混合优化算法,增加两层无解方案的排除过程以降低算法冗余;最后,借助航天任务工具箱(Aero-space Tool Kit,ATK)的机动规划序列段脚本工具对该方法进行软件化实现仿真.结果表明,该方法能在确保计算结果正确的同时提升效率,显著降低目标航天器调相机动规划问题的求解时间.

Aiming at the phasing maneuver programming of rendezvous and docking mission be-tween target spacecraft and chaser spacecraft,an optimization method of target spacecraft phasing maneuver strategy considering variable constraints for orbital rendezvous mission is proposed.First,based on modeling nonlinear programming problems and analyzing specific constraints,the variable constraints that are generated during orbit prediction are transformed into fixed con-straints.Second,the hybrid optimization algorithm combining DC and SQP incorporates two layers of enhanced process to eliminate unsolvable solutions and reduce algorithm redundancy.Fi-nally,the method was implemented and simulated using the maneuver planning sequence script tool in ATK.Results demonstrate that the proposed approach not only ensures computational ac-curacy but also enhances efficiency and significantly reduces the solution time for phasing maneuver planning of target spacecraft.

商铭彦;金柯;杨震;罗亚中;范高洁;商帅

国防科技大学空天科学学院·长沙·410073||太空系统运行与控制全国重点实验室·长沙·410073国防科技大学空天科学学院·长沙·410073||太空系统运行与控制全国重点实验室·长沙·410073国防科技大学空天科学学院·长沙·410073||太空系统运行与控制全国重点实验室·长沙·410073国防科技大学空天科学学院·长沙·410073||太空系统运行与控制全国重点实验室·长沙·410073北京空间飞行器总体设计部·北京·100094北京空间飞行器总体设计部·北京·100094

航空航天

目标航天器轨道调相可变约束纬度幅角微分修正序列二次规划

target spacecraftorbital phasingvariable constraintargument of latitudedifferential cor-rectionsequential quadratic programming

《飞控与探测》 2026 (2)

10-20,11

国家自然科学基金(12432017,12372052)载人航天工程科技创新团队

10.20249/j.cnki.2096-5974.2026.02.002

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