首页> 外文会议>International Symposium on Space Flight Dynamics >MARS RECONNAISSANCE ORBITER AEROBRAKING DAILY OPERATIONS AND COLLISION AVOIDANCE
【24h】

MARS RECONNAISSANCE ORBITER AEROBRAKING DAILY OPERATIONS AND COLLISION AVOIDANCE

机译:火星侦察轨道轮充氧每日运营和碰撞避免

获取原文

摘要

The Mars Reconnaissance Orbiter reached Mars on March 10, 2006 and performed a Mars orbit insertion maneuver of 1 km/s to enter into a large elliptical orbit. Three weeks later, aerobraking operations began and lasted about five months. Aerobraking utilized the atmospheric drag to reduce the large elliptical orbit into a smaller, near circular orbit. At the time of MRO aerobraking, there were three other operational spacecraft orbiting Mars and the navigation team had to minimize the possibility of a collision. This paper describes the daily operations of the MRO navigation team during this time as well as the collision avoidance strategy development and implementation.
机译:Mars侦察轨道运动员于2006年3月10日达到火星,并进行了1公里/秒的火星轨道插入机动进入一个大型椭圆轨道。 三周后,机会业务开始并持续了大约五个月。 有气速使用大气阻力,以将大型椭圆轨道减小到较小的圆形轨道上。 在MRO Aerobraking时,有三个其他操作航天器轨道轨道火星,导航团队必须尽量减少碰撞的可能性。 本文介绍了在此期间MRO导航团队的日常运营以及碰撞避免战略开发和实施。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 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