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Spatial small aircraft formation flying control system

A formation flight and control system technology, applied in the field of space small aircraft, can solve the problem of insufficient ability of a single aircraft to perform space missions, and achieve the effects of improving system adaptability, broad application prospects, and low cost

Inactive Publication Date: 2014-12-17
BEIJING AEROSPACE INST OF THE LONG MARCH VEHICLE +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The technical problem solved by the present invention is: aiming at the insufficient ability of a single aircraft to perform space tasks, a small space aircraft formation flight control system is proposed, which realizes the cooperative operation of multiple space small aircraft and improves combat effectiveness

Method used

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  • Spatial small aircraft formation flying control system

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Embodiment Construction

[0023] The present invention will be described below in conjunction with the accompanying drawings.

[0024] Due to mission requirements, the aircrafts in the formation often need to keep their relative positions in the formation basically unchanged. The general keeping strategy is that each small space vehicle in the formation keeps the relative position of the reference point in the formation unchanged. The present invention adopts the keeping strategy with the main aircraft as the agreed point, also known as follow and keep. When the number of small space vehicles is small, centralized control is adopted, that is, the position of each small space vehicle in the formation relative to the main vehicle remains unchanged, Figure 2a It is a schematic diagram of a formation flight composed of a master aircraft and two slave aircraft. In the figure, the positions of the two slave aircraft relative to a master aircraft remain unchanged; when the number of space small aircraft is l...

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Abstract

The invention discloses a spatial small aircraft formation flying control system. The spatial small aircraft formation flying control system comprises a task planning system, a formation calculation module, a primary aircraft control module, a formation pattern control module and a secondary aircraft control module, wherein the task planning module is used for sending a mission spatial characteristic and a target characteristic to the formation calculation module; the formation calculation module determines the optimal formation pattern of the spatial small aircrafts and sends the optimal formation pattern to the formation pattern control module; the task planning module is also used for sending a commanded flying state to the primary aircraft directly; the primary aircraft control module performs flying control to obtain a practical motion state; the formation pattern control module calculates to obtain a commanded motion state of a secondary aircraft and sends the calculation result to the secondary aircraft control module; the secondary aircraft control module performs flying control to obtain the practical motion state.

Description

technical field [0001] The invention relates to a small space vehicle, in particular to a formation flight control system of the small space vehicle. Background technique [0002] Spacecraft formation flight is a new space operation mode of spacecraft that emerged in the late 1990s with the development of computer technology, new materials, and new energy technologies. In the center force field, multiple spacecraft with the same orbital period fly close to each other, and can form a specific relative motion orbit with each other. The spacecraft cooperate with each other and are closely connected to form a large "virtual satellite" in a distributed manner. (or "distributed satellite system", "distributed spacecraft system"), resulting in the so-called "emergence" phenomenon in system theory, and its performance far exceeds that of the traditional single spacecraft system. Due to the broad application prospects of spacecraft formation flight in the fields of detection and com...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B19/418
Inventor 陈垦梁海朝王永海水涌涛刘佳琪孟刚
Owner BEIJING AEROSPACE INST OF THE LONG MARCH VEHICLE
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