X-ray pulsar navigation embedded simulation system based on semiconductor laser
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- XIDIAN UNIV
- Publication Date
- 2009-12-23
- Estimated Expiration
- Not applicable · inactive patent
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Abstract
Description
technical field
[0001] The invention belongs to the technical field of navigation, and in particular relates to an X-ray pulsar navigation simulation system, which is used for simulating the autonomous celestial navigation of an orbiting spacecraft based on the X-ray pulsar. Background technique
[0002] Navigation and positioning based on X-ray pulsars is a celestial navigation method that uses X-ray pulsar radiation pulse arrival time measurement as information input, which can provide position, velocity, time, attitude, etc. for near-earth, deep space and interstellar space spacecraft. Rich navigation information. The pulsar-based navigation technology was first proposed by Dr. Durns of the Jet Propulsion Laboratory in the United States in 1974; in 1981, Chester and Bateman of the Institute of Communications Systems of the United States proposed the use of pulsar X-ray sources for spacecraft navigation. Conception; in 1999, the US Air Force's "Advanced Research and Globa...