首页> 外文会议>AAS/AIAA spacefilght mechanics meeting >Precession of angular momentum cone in free pitch tumble of radarsat in orbit
【24h】

Precession of angular momentum cone in free pitch tumble of radarsat in orbit

机译:角动量锥在进场雷达的自由俯仰翻转中的进动

获取原文

摘要

The attitude and attitude rate telemetry during free pitch tumble of RADARSAT in June 1997 is examined. The cone axis of the satellite angular momentum vector, during free rotation of the satellite about the pitch axis, was in precession almost synchronously with the sun-synchronous orbital plane of the satellite.
机译:考察了1997年6月RADARSAT在自由俯仰过程中的姿态和姿态速率遥测。在卫星绕俯仰轴自由旋转期间,卫星角动量矢量的圆锥轴几乎与卫星的太阳同步轨道平面同步进动。

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