A six-degree-of-freedom fixed-time rendezvous and docking control method for spacecraft

A technology of rendezvous and docking, fixed time, applied in the direction of adaptive control, general control system, control/regulation system, etc., can solve the problems of parameter estimated value and actual value deviation, parameter overestimation, strong conservatism, etc.
CN108427281BActive Publication Date: 2020-04-21BEIHANG UNIV

Patent Information

Authority / Receiving Office
CN ยท China
Patent Type
Patents(China)
Current Assignee / Owner
BEIHANG UNIV
Publication Date
2020-04-21

Smart Images

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

Abstract

The invention discloses a six-degree-of-freedom fixed-time rendezvous docking control method for a spacecraft. Installation errors of a booster are taken into consideration. The method comprises the steps that under the situation that the installation errors of the booster existing in a service spacecraft are taken into account, a six-degree-of-freedom rendezvous docking motion model of the service spacecraft and a rolling target spacecraft is constructed, wherein the model comprises the motion descriptions of the relative position and relative attitude between the two spacecrafts; based on the established rendezvous docking motion model in which the installation errors of the booster are taken into account, and by using related motion variations, a new fixed time sliding surface is obtained; a fixed time rendezvous docking controller is obtained based on the sliding surface, and an installation error angle of the booster is estimated by constructing new adaptive rules. The method hasthe advantages of fixed time characteristics, high controlling precision, parameter overestimation preventing and the like, and the method is suitable for a six-degree-of-freedom spacecraft rendezvousdocking control mission with higher timeliness demands.
Need to check novelty before this filing date? Find Prior Art

Description

technical field

[0001] The invention relates to the technical field of spacecraft control, and is mainly applied to six-degree-of-freedom motion control in spacecraft rendezvous and docking, and specifically relates to a spacecraft six-degree-of-freedom fixed-time rendezvous and docking control method considering thruster installation deviation. Background technique

[0002] At present, with the development of aerospace technology, countries have launched a large number of spacecraft. How to realize the rendezvous and docking of the service spacecraft and the tumbling target spacecraft is an important guarantee for the service spacecraft to complete on-orbit maintenance. At the same time, rendezvous and docking operations often have time constraints, requiring the completion of related tasks within a certain period of time; in addition, considering that there are propeller installation deviations in the service spacecraft in practice, the Six Freedoms during the rendezvous 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