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Spacecraft flight control method and device, storage medium and processor

A flight control and spacecraft technology, which is applied in the field of spacecraft measurement and control, can solve the problems of poor timeliness of spacecraft flight control, and the flight control effect is difficult to meet expectations, and achieves the effect of improving timeliness and improving flight control effect.

Pending Publication Date: 2022-05-17
BEIJING AEROSPACE CONTROL CENT
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0006] The main purpose of this application is to provide a spacecraft flight control method and device, storage medium and processor, to solve the large-loop closed-loop control mode of measurement and control station-spacecraft-measurement and control station and the coupling of uplink and downlink measurement and control links in related technologies The control method has poor timeliness for the flight control of the spacecraft under the condition of large delay, which leads to the problem that the flight control effect is difficult to meet expectations

Method used

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  • Spacecraft flight control method and device, storage medium and processor
  • Spacecraft flight control method and device, storage medium and processor
  • Spacecraft flight control method and device, storage medium and processor

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Embodiment Construction

[0032] It should be noted that, in the case of no conflict, the embodiments in the present application and the features in the embodiments can be combined with each other. The present application will be described in detail below with reference to the accompanying drawings and embodiments.

[0033] In order to enable those skilled in the art to better understand the solution of the present application, the technical solution in the embodiment of the application will be clearly and completely described below in conjunction with the accompanying drawings in the embodiment of the application. Obviously, the described embodiment is only It is an embodiment of a part of the application, but not all of the embodiments. Based on the embodiments in this application, all other embodiments obtained by persons of ordinary skill in the art without creative efforts shall fall within the scope of protection of this application.

[0034] It should be noted that the terms "first" and "second...

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Abstract

The invention discloses a spacecraft flight control method and device, a storage medium and a processor. The method comprises the following steps: when a flight control event is detected, determining light traveling time between a target spacecraft and a target measurement and control station; determining the sending time of the target uplink carrier according to the optical line time and the planned execution time of the target control instruction; according to the sending time of the target uplink carrier and a preset duration, the target control instruction is sent to the target spacecraft, and the preset duration is smaller than the transmission time of the uplink carrier from the target measurement and control station to the target spacecraft; and performing flight control on the target spacecraft according to the target control instruction. According to the method and the device, the problem that the flight control effect is difficult to conform to expectation due to the fact that the flight control timeliness of the spacecraft under the large time delay working condition is poor by adopting a measurement and control station-spacecraft-measurement and control station large-loop closed-loop control mode and an uplink and downlink measurement and control link coupling control mode in the related technology is solved.

Description

technical field [0001] The present application relates to the technical field of spacecraft measurement and control, in particular, to a spacecraft flight control method and device, a storage medium, and a processor. Background technique [0002] According to the flight control requirements of the spacecraft, the uplink remote control command or data injection is carried out to the spacecraft through the measurement and control station, and then the status monitoring and interpretation of the execution effect of the remote control command is carried out through the downlink telemetry forwarded by the measurement and control station. For example, in the flight control mission of near-Earth or lunar probes, due to the short distance between the spacecraft and the measurement and control station, from the sending of the remote control command on the ground to the receipt of the execution state change of the on-board command forwarded by the measurement and control station in res...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10
CPCG05D1/101
Inventor 金文马李剑润冬程艳合张爱成赵焕洲王成崔晓峰乔宗涛
Owner BEIJING AEROSPACE CONTROL CENT
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