| 1. | Algorithm and simulation of autonomous orbit determination for navigation satellites
导航卫星自主定轨的算法研究及模拟结果 |
| 2. | Simulation of impact of force models on orbiting accuracy of reduced - dynamic orbit determination
的弹道导弹攻防对抗仿真系统建模研究 |
| 3. | Kinematic orbit determination of low - earth orbiters based on gps precise point positioning technique
精密单点定位的低轨卫星几何法定轨 |
| 4. | Application of the improved helmert method for variance component estimation in precise orbit determination
方差分量估计方法在精密定轨中的应用 |
| 5. | 6 . initial orbit determination for satellites based on angle measurements is investigated
对茧于纯角度观测倩息的卫星轨邀确定方法进行了研究。 |
| 6. | Autonomous relative orbit determination for satellite formation flying on basis of orbit element differences
基于轨道根数差的卫星编队自主定轨研究 |
| 7. | The changing law is presented , which can improve satellite autonomous orbit determination precision
总结了其变化规律，可用于提高卫星自主定轨精度。 |
| 8. | 2 . using the startlight angle as measurements , extended kalman filter is used for orbit determination
以星光角距为量测量，运用广义卡尔曼滤波实现定轨。 |
| 9. | An autonomous satellite attitude and orbit determination system based on the stellar refraction measurement is described
摘要研究了基于星光折射量测进行自主确定卫星姿态及轨道的方法。 |
| 10. | Algorithms of on - board gps real - time single point positioning and dynamic orbit determination using positioning solutions are mainly studied
本文重点研究星载gps单点实时定位和基于单点定位结果的动力学定轨方法。 |
