Finite-time posture fault-tolerant control method for spacecraft formation

A limited-time, fault-tolerant control technology, applied in the field of multi-spacecraft formation flight, can solve problems such as unknown and momentary changes in spacecraft inertia, and achieve the effects of short coordination time, simple structure and high control precision
CN109459931AInactive Publication Date: 2019-03-12NANJING UNIV OF SCI & TECH

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 1
  • Figure 2
    Figure 2
  • Figure 3
    Figure 3
Patent Text Reader

Abstract

The invention relates to a finite-time posture fault-tolerant control method for a spacecraft formation and belongs to the technical field of multi-spacecraft formation flying. In order to reduce communication paths and avoid resource waste, a directional communication topological structure with small communication traffic is adopted between spacecraft formation members; in addition, in order to make a spacecraft formation posture control system achieve synergy more quickly and stably, the finite-time posture fault-tolerant control method for the spacecraft formation is provided on the basis of a finite-time algorithm with high robustness and fast convergence, a redundant fault-tolerant algorithm with better fault-tolerant performance and an self-adaptive algorithm with a good suppressioneffect on system uncertainty and interference. According to the method, a limited-capacity self-adaptive posture cooperative tracking fault-tolerant control strategy is perfected, a redundant fault-tolerant control method is achieved through reasonable torque distribution, and at the same time, a self-adaptive law is designed for reducing the influence of inertia variation and interference; moreover, fast convergence of a spacecraft cooperative tracking error system can be realized, and the robustness and practicability of the control system are further improved.
Need to check novelty before this filing date? Find Prior Art

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 ...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More