PIO-based round orbital space vehicle formation reconfiguration type anti-collision path planning method

Abstract

The invention discloses a PIO-based round orbital space vehicle formation reconfiguration type anti-collision path planning method, and belongs to the technical field of space vehicle attitude control. According to the algorithm, firstly, a spaceflight short-distance relative motion linear C-W equation is used for dynamics modeling; then, a space vehicle formation discrete dynamic equation is usedfor calculating the total fuel consumption of the space vehicle formation; an infinite series method is used for calculating the collision probability between the space vehicles; a corresponding fitness function is built through an exterior penalty function method; then, a self-adaptive geomagnetic factor coefficient is introduced; the original global search and local search capability of the deterrent algorithm is balanced; the flight optimization path considering the fuel consumption and avoiding collision is finally obtained. The algorithm is simple; the formation fuel consumption and collision avoidance factors between the space vehicles are considered under the condition of given initial and final space vehicle formation; the optimization of the space vehicle formation flight path isrealized.

Description

technical field [0001] The invention discloses a PIO (Pigeon-Inspired Optimization, pigeon-inspired optimization) circular orbit spacecraft formation reconfiguration anti-collision path planning method, belonging to the technical field of spacecraft attitude control. Background technique [0002] Satellite autonomous swarm formation flight has been proven as a feasible technology in NASA and U.S. Air Force missions. By using a formation composed of smaller and more agile spacecraft, the length of the observation baseline can be increased, and the redundancy and reconfiguration of the system can be improved, which is conducive to the realization of more demanding space missions and failures under harsher conditions. detection. Today, the focus on applications such as spacecraft interferometric ground imaging, spacecraft navigation and guidance, synthetic aperture radar and military reconnaissance makes the research on spacecraft formation technology more and more important. ...

AI Technical Summary

Problems solved by technology

[0004] The purpose of the invention of the present invention is to address the deficiencies of the above-mentioned background technology, providing a PIO-based circular orbit spacecraft formation reconfiguration anti-collision path planning method, considering the formation fuel Consumption and collision avoidance factors between spacecraft realize the optimization of the flight path of the spacecraft formation, and solve the technical problem of complex calculation when the existing spacecraft formation is reconfigured to avoid collision planning

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