随着通信卫星液体双组元推进系统的日益广泛应用、卫星稳定问题越来越复杂、越来越严重。本文根据国外有关文献报道,简述了地球静止轨道卫星的稳定问题。主要是从以下几个飞行阶段的卫星稳定问题进行讨论,即停泊轨道阶段(从卫星离开航天飞机货舱到近地点发动机点火)、转移轨道阶段 With the increasingly wide application of bi-component propulsion system for communications satellites, the problem of satellite stability is more and more complicated and more and more serious. This article describes the stability of geostationary satellites based on reports from abroad. The discussion is mainly focused on the issue of satellite stabilization in the following phases of flight: the phase of the orbital orbit (the ignition of the engine from the spacecraft leaving the space shuttle to the perigee), the transitional orbit phase