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A Method for Autonomous Orbit Replanning of Space Vehicle

A space vehicle, autonomous orbit technology, applied in instruments, adaptive control, control/regulation systems, etc., can solve problems such as large manpower and material costs, inability to re-plan orbits, safety accidents, etc., to reduce manpower and material costs and improve tasks. Adaptability, effectiveness in reducing security risks

Active Publication Date: 2019-06-18
BEIJING AEROSPACE AUTOMATIC CONTROL RES INST +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Traditional space transport vehicles, such as launch vehicles, are launched at one time and left unattended after take-off, that is, if they encounter engine failure or other unexpected situations after take-off, they can only resign themselves to their fate and cannot re-plan their orbits, so they do not have the ability to recover from failures , so in the case of a fault, it will often cause a large economic loss, and even a safety accident
Although some aircraft have the ability to re-orbit and have the function of failure recovery, (such as satellites, etc., when the rocket fails to send it into the predetermined orbit or there is a large orbital deviation, it will receive instructions from the ground to inject and upload to re-orbit. planning) but they are all re-planned based on the space-ground communication mode, that is, orbit re-planning instructions are generated on the ground in the event of a fault, and uploaded to the aircraft through remote control. This method requires ground measurement and control equipment and a large number of technical personnel to support it. On the other hand, it is also limited by the measurement and control arc section and the space-ground communication situation. When some faults occur in the measurement and control blind area or when there is a space-ground communication failure, the aircraft will still be unable to receive ground commands and the failure cannot be rescued.

Method used

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  • A Method for Autonomous Orbit Replanning of Space Vehicle
  • A Method for Autonomous Orbit Replanning of Space Vehicle
  • A Method for Autonomous Orbit Replanning of Space Vehicle

Examples

Experimental program
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Effect test

Embodiment 1

[0042] If the base-stage launch vehicle motor fails, the thrust drop does not put the spacecraft into orbit. The aircraft enters the taxiing segment and collects the status information of the spacecraft:

[0043] project

[0044] According to the state information, calculate the number of orbital elements, where |a-a 0 |=2350kmΔa=100km, so the judgment result is that the orbit parameters are out of tolerance, and orbit re-planning is required

[0045] According to the state parameters and the orbit parameter database, select the new orbit parameters and get iresult=3, that is, select the third re-planned orbit, that is, the following figure 1 The spacecraft in the new target orbit, the new target orbit is selected successfully, the spacecraft needs to enter the following new orbit:

[0046] Table 1: New target orbits for spacecraft

[0047]

[0048]

[0049] If trajectory re-planning is not performed at this time, the spacecraft still adopts the original par...

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Abstract

The invention relates to an autonomous orbit reprogramming method of a spaceflight aircraft. The method comprises the following steps that spacecraft state information is acquired; out-of-tolerance of an orbit is calculated according to the state information; whether reprogramming is performed is judged according to the out-of-tolerance situation, flying according to the normal default orbit is performed if the out-of-tolerance situation does not occur, and ballistic reprogramming is performed if the out-of-tolerance situation occurs; the minimum i value corresponding to an accessible target orbit parameter in an orbit parameter library is judged according to the order of priority, and the preselected orbit corresponding to the minimum i value acts as a new target orbit; and the aircraft is controlled to fly according to the new target orbit. The spaceflight aircraft is creatively enabled to have the autonomous orbit reprogramming capacity so that self-rescuing under the fault state can be realized, the expected target is completed under the fault situation and the economic loss can be reduced and the safety risk can be reduced; and the manpower and material resource cost can be reduced through the autonomous mode without depending on ground equipment and personnel.

Description

technical field [0001] The invention relates to an autonomous orbit re-planning method for a space vehicle, belonging to the field of space vehicle guidance and control. Background technique [0002] Traditional space transport vehicles, such as launch vehicles, are launched once and left alone after take-off, that is, if they encounter engine failure or other unexpected situations after take-off, they can only resign themselves to their fate and cannot re-plan their orbits, so they do not have the ability to recover from failures , so in the case of failure, it will often cause greater economic losses, and even safety accidents will occur. Although some aircraft have the ability to re-orbit and have the function of failure recovery, (such as satellites, etc., when the rocket fails to send it into the predetermined orbit or there is a large orbital deviation, it will receive instructions from the ground to re-orbit. planning) but they are all re-planned based on the space-g...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B13/04
CPCG05B13/042
Inventor 李超兵王晋麟禹春梅徐国强祁琪吕建强
Owner BEIJING AEROSPACE AUTOMATIC CONTROL RES INST
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