基于惯性/天文深度融合的跨域飞行器异构多源组合导航方法

doi:10.7527/S1000-6893.2024.30614

Abstract

Abstract:

China plans to achieve airline-flight-mode space transportation between ground and orbit， as well as between orbit and orbit by 2045. Cross domain vehicles， due to their ability to cross speed， airspace， and media domains， can achieve flight-based back-and-forth transportation between space and earth. Their special strategic value have been highly valued by countries around the world. The flight process of cross domain vehicles requires multiple high-speed and complex flight stages， which puts higher requirements on the reliability and safety of navigation systems. Therefore， there is an urgent need to develop autonomous navigation methods for cross domain vehicles for airline-flight-mode space transportation. To address this issue， this paper proposes a heterogeneous multi-source integrated navigation method for cross domain vehicles based on inertial/celestial deep fusion to solve the autonomous navigation problem of cross domain vehicles in achieving flight oriented space transportation. The results show that the method proposed can fully utilize the complementary advantages of inertial navigation and celestial navigation， correct navigation errors， effectively improve the output accuracy and reliability of cross domain vehicles navigation systems in complex flight environments， ensure the safe and reliable operation of navigation systems of cross domain vehicles， and enhance their seamless information fusion ability in the entire flight stage， accumulating technologies for realizing the concept of airline-flight-mode space transportation.

Key words: cross domain vehicle, celestial navigation, performance evaluation, deep fusion of information, navigation system

CLC Number:

V249

Xinrui ZHANG, Zhi XIONG, Bing HUA, Jun KANG, Huiyu HE. A heterogeneous multi-source integrated navigation method for cross-domain vehicles based on inertial/celestial deep fusion[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(S1): 730614.

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传感器误差项	数值
陀螺零偏/（°）	0.003
陀螺一阶马尔可夫过程/（°）	0.003
加速度计零偏/（10^-4g）	1
星敏感器角度输出误差/（"）	3

导航误差项		数值
位置误差/m	经度	19.116 5
	纬度	17.094 0
	高度	8.682 7
姿态误差/（"）	横滚	3.841 8
	俯仰	1.061 0
	航向	3.808 4

导航误差项		数值
位置误差/m	经度	232.330 0
	纬度	110.720 5
	高度	77.300 9
姿态误差/（"）	横滚	174.507 1
	俯仰	13.962 8
	航向	184.751 5

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A heterogeneous multi-source integrated navigation method for cross-domain vehicles based on inertial/celestial deep fusion

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