An optimal trajectory design method considering the constraint of a non-cooperative target no-fly zone
A non-cooperative target, design method technology, applied in the field of optimal orbit design considering the constraints of non-cooperative target no-fly zone
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0093] The present invention is described in further detail below in conjunction with accompanying drawing:
[0094] Such as figure 1 As shown, the optimal orbit design method of the non-cooperative target no-fly zone constraint considered in the present invention comprises the following steps:
[0095] 1) Establish the earth’s inertial coordinate system EXYZ and the target spacecraft’s orbital coordinate system Txyz. The tracking spacecraft and the target coordinate system are on the same orbit. In the initial state, the phase angle of the tracking spacecraft lagging behind the target spacecraft is α. Set the target The no-fly zone of the spacecraft body and the no-fly zone of the target spacecraft sensor;
[0096] 2) Establish the orbital model of the relative motion of the spacecraft, seek the solution of the orbital model of the relative motion of the spacecraft, and then eliminate the drift item according to the properties of the solution of the orbital model of the rela...
PUM
Abstract
Description
Claims
Application Information
- R&D Engineer
- R&D Manager
- IP Professional
- Industry Leading Data Capabilities
- Powerful AI technology
- Patent DNA Extraction
Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.
© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com