首页> 中文期刊>火力与指挥控制 >基于冲量法实现航天器编队重构控制仿真的研究

基于冲量法实现航天器编队重构控制仿真的研究

     

摘要

Spacecraft Formation reconstructed for visibility is not strong,proposes to impulse a spacecraft formation reconstructed visual simulation technology. Double pulse motor is the transfer of the spacecraft space near orbit that it needs two impulse maneuver. Application of the principle of relative motion between the spacecraft,space target orbit six elements as the objective function space target by adjusting the orbital parameters of the spacecraft formation reconfiguration,swing around the fly transferred to swing hanging around the fly,and then come to the transfer of spacecraft the swing hanging around fly formation to the basic relationship of the impulse required to achieve control of the spacecraft space target formations reconstruction.%针对航天器编队重构的可视性不强,提出一种冲量法实现航天器编队重构的视景仿真技术。双脉冲机动是指航天器对空间目标的近轨道转移时,所需要的两次冲量机动。应用航天器之间相对运动原理,以空间目标轨道六要素为目标函数,通过调整航天器轨道参数对空间目标进行编队重构,有摆动绕飞转移至摆动式悬挂绕飞,进而得出了航天器转移摆动式悬挂绕飞编队到所需冲量基本关系,从而实现航天器对空间目标进行编队重构控制。

著录项

相似文献

  • 中文文献
  • 外文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号