Finite-time posture fault-tolerant control method for spacecraft formation
Patent Information
- Authority / Receiving Office
- CN · China
- Current Assignee / Owner
- NANJING UNIV OF SCI & TECH
- Publication Date
- 2019-03-12
- Estimated Expiration
- Not applicable · inactive patent
Smart Images

Figure 1 
Figure 2 
Figure 3
Abstract
Description
technical field
[0001] The invention belongs to the technical field of multi-spacecraft formation flight, in particular to a space vehicle formation limited-time attitude fault-tolerant control method. Background technique
[0002] Spacecraft formation flight is a main mode of spacecraft group work, and spacecraft attitude coordination is an important basis for spacecraft formation flight. Focus distance, synthetic aperture, occlusion by special celestial bodies, or convergence of weak target signals in the deep distance can not be completed by a single spacecraft. Against this background, the research on multi-spacecraft formation flight has developed rapidly and has become one of the research hotspots in recent years.
[0003] With the deepening of human research in the field of spaceflight, more and more complex space missions are put into engineering practice, and the time or coordination rate required for multi-spacecraft to complete attitude coordination has become an ...