首页|期刊导航|空间控制技术与应用|鹊桥二号中继星自主角动量管理设计及实现

鹊桥二号中继星自主角动量管理设计及实现OA北大核心CSTPCD

Design and Application of Momentum Management for Queqiao-2 Relay Satellite

中文摘要英文摘要

针对鹊桥二号中继星动量轮喷气卸载对使命轨道的扰动及卫星长寿命的影响,提出一种自主角动量管理策略.建立基于卫星姿态机动的角动量预测模型,给出角动量变化趋势,避免卫星机动过程动量轮出现饱和问题.基于角动量积累规律和中继通信任务需求提出了事件触发的角动量管理策略,通过卫星姿态规划减少角动量积累,有效增大喷气卸载周期.利用对称喷气方式实现卸载,有效减少喷气对轨道的干扰,提高轨道维持的稳定性.试验和在轨结果验证了策略的自主性和有效性.

An autonomous momentum management strategy is proposed to solve the problems of the disturbance to the mission orbit and the influence on long-life of the Queqiao-2 relay satellite,which caused by the momentum wheel unloading under the control of thrust.Firstly,a momentum predictive model based on the satellite's attitude maneuver is established to predict the satellite's momentum changes,avoiding the problem of momentum wheel sat-uration during satellite maneuvering.Secondly,an event-triggering momentum management strategy is used to a-chieve autonomous management of the relay satellite on orbit momentum,increasing the jet unloading period effec-tively.In addition,the coupling jet unloading is adopted to improve the stability of obit maintenance.Finally,the experiments and flight results verify the effectiveness of the proposed momentum management strategy.

郝策;王勇;关轶峰;王洪斌;胡少春;张迎发;郑永洁;韩沛宏

北京控制工程研究所,北京 100094||燕山大学,秦皇岛 066004北京控制工程研究所,北京 100094北京控制工程研究所,北京 100094燕山大学,秦皇岛 066004北京控制工程研究所,北京 100094北京控制工程研究所,北京 100094北京控制工程研究所,北京 100094北京控制工程研究所,北京 100094

鹊桥二号中继星预测模型角动量管理角动量卸载

Queqiao-2 relay satellitepredictive modelmomentum managementmomentum wheel unloading

《空间控制技术与应用》 2024 (6)

42-49,8

国家重大专项工程探月四期 Major National Projects of China(The 4th Stage of China's Lunal Exploration)

10.3969/j.issn.1674-1579.2024.06.005

评论