1) space guidance
航天制导
2) spacecraft guidance
航天器制导
3) spacecraft navigation and control
航天器制导与控制
4) spacecraft navigation
航天器导航
1.
The applications of the pulsar TOA transfer equation to the spacecraft navigation using pulsars are discussed.
较详细地介绍了脉冲星脉冲到达时间(TOA)转换方程,讨论了脉冲星TOA转换方程在航天器导航算法中的具体应用问题。
5) celestial navigation
天文导航
1.
Survey of overseas celestial navigation technology development;
国外天文导航技术发展综述
2.
Analysis of observability and the degree of observability in autonomous celestial navigation;
航天器自主天文导航系统的可观测性及可观测度分析
3.
Design Scheme for the Marine Celestial Navigation System Based on the ECDIS System;
基于ECDIS系统的舰船天文导航系统的设计方案
6) celestial navigation system
天文导航
1.
Based on the ideal of making most use of the celestial navigation system(CNS) that is high accuracy,after analyzing the principle and error models of the CNS and inertial navigation system(INS),an error correction algorithm of the CNS/INS integrated navigation is presented.
通过分析导弹天文导航和惯性导航的导航原理和误差模型,在基于充分利用高精度天文导航参数的思想上,提出了组合导航的误差修正方法。
补充资料：波束制导(见遥控制导)
波束制导(见遥控制导)
beam-rider guidance
boshu zhidao波束制导(beam一rider guidanee)见遥控制导。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条