Space interception guidance with uncertain factors
Abstract
Based on the interception manifold concept, a method is proposed for treating the interception guidance problem of a modern space vehicle with uncertain factors and any proper acceleration. The method in a sense is a generalization of the classical mode; it is simple and seems to satisfy various trajectory reuirements of the guidance process.
- Publication:
-
China Rept Sci Technol JPRS CST
- Pub Date:
- October 1984
- Bibcode:
- 1984ChRST.......44S
- Keywords:
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- Interception;
- Missile Control;
- Pursuit Tracking;
- Spacecraft Tracking;
- Trajectory Control;
- Acceleration (Physics);
- Error Analysis;
- Optimal Control;
- Position Errors;
- Astrodynamics