航天器工程2026，Vol.35Issue(4)：53-60,8.DOI:10.3969/j.issn.1673-8748.2026.04.008
基于多目标优化的航天器姿态辅助热控制方法研究
A Spacecraft Attitude-assisted Thermal Control Method Based on Multi-objective Optimization
摘要
Abstract
Conventional spacecraft thermal control systems feature high power consumption,com-plexity,and limited environmental adaptability.A dynamic attitude-assisted thermal-control method based on multi-objective optimization is proposed in this paper.A coupled model of the spacecraft orbital thermal environment and attitude is established.The effects of external heat fluxes are considered.They include direct solar radiation,Earth infrared radiation,and Earth al-bedo radiation.A complete energy-balance equation is derived.A multi-objective cost function is formulated.Temperature variance,temperature change rate and attitude variation are taken as optimization objectives.Constraints cover attitude angles,angular velocity,solar-array orienta-tion,and temperature safety.Online optimization is implemented using a receding-horizon opti-mization framework and a sequential quadratic programming algorithm.Simulation results show that compared with the conventional mode alternating between Sun-pointing and Earth-gazing at-titudes of the Z-face,the proposed method reduces the spacecraft temperature variation range by approximately 14℃.It effectively relieves the burden on the thermal-control system.This meth-od provides a theoretical basis and a technical approach for integrated attitude-orbit-thermal control.关键词
航天器热控制/姿态机动/多目标优化/外热流计算Key words
spacecraft thermal control/attitude maneuver/multi-object optimization/external heat-flux calculation分类
航空航天引用本文复制引用
孙博文,矫媛媛,潘晓刚,李禾雄..基于多目标优化的航天器姿态辅助热控制方法研究[J].航天器工程,2026,35(4):53-60,8.基金项目
国家自然科学基金(62503487) （62503487）
航天器热控全国重点实验室开放基金(NKLST-JJ-202401005) （NKLST-JJ-202401005）
