Spacecraft momentum dumping using gravity gradient

被引：5

作者：

Tong, D ^{[1
]}

机构：

[1] Boeing Co, Boeing Informat Space & Def Syst, Seattle, WA 98124 USA

来源：

JOURNAL OF SPACECRAFT AND ROCKETS | 1998年 / 35卷 / 05期

关键词：

D O I：

10.2514/2.3389

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The disturbance angular momentum accumulated by the momentum wheels or control momentum gyros onboard an orbiting spacecraft can be alleviated with gravity-gradient torque in some cases. How a modification to the nominal spacecraft operational attitude profile can result in lowering propellant consumption, potentially extending the spacecraft's life span on orbit, is discussed. The feasibility of using gravity gradient for momentum dumping is demonstrated in a case study.

引用

页码：714 / 717

页数：4

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