摘要
运用全程测控模型,对卫星或飞船的运行轨道与地球赤道平面有固定夹角情况下,全程测控所需最少站点的个数进行研究。分别从夹角为0°、90°和其余情况3个方面给出结果,并在此基础上指出模型改进的方向。
Using full monitoring and control model, under the condition of the satellite or spacecraft orbit the Earth equatorial plane with a fixed angle case, the entire monitoring and control at least the required number of sites were studied. Respectively, from an angle of zero, ninety, and the remaining cases the results are given in three aspects, and on this basis the direction of the model is improved.
出处
《黑龙江工程学院学报》
CAS
2011年第4期76-78,共3页
Journal of Heilongjiang Institute of Technology
