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Space rendezvous and docking laser radar scanning tracking control system and method

A technology of scanning and tracking and laser radar, which is applied in the field of space rendezvous and docking laser radar scanning and tracking control system, can solve the problems of high cost, heavy weight, and complicated control of two-axis control systems, and achieve improved system reliability and simplified circuit and structure Effect

Pending Publication Date: 2021-06-04
INST OF OPTICS & ELECTRONICS - CHINESE ACAD OF SCI
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  • Abstract
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  • Application Information

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Problems solved by technology

Therefore, the existing two-axis control system is relatively complicated to control, high in cost, heavy in weight, and has the problem of adaptability to the space environment.

Method used

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  • Space rendezvous and docking laser radar scanning tracking control system and method
  • Space rendezvous and docking laser radar scanning tracking control system and method
  • Space rendezvous and docking laser radar scanning tracking control system and method

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Embodiment Construction

[0070] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0071] The object of the present invention is to provide a space rendezvous and docking lidar scanning and tracking control system and method, which can reduce system cost and weight and improve system reliability while meeting precision requirements.

[0072] In order to make the above objects, features and advantages of the present invention more comprehensible, the present invention will be further described in detail below in conjunction with the accompanyi...

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Abstract

The invention discloses a space rendezvous and docking laser radar scanning tracking control system and method. A single-chip DSP is used for establishing a closed-loop control system, and the motion directions and frequency division coefficients of two stepping motors are determined according to the azimuth axis angle value, the pitch axis angle value and the two-dimensional miss distance. The single-chip FPGA is adopted to realize SPWM subdivision driving of stepping motors of a pitch axis and an azimuth axis, and a pitch axis SPWM wave and an azimuth axis SPWM wave are generated according to the motion directions and frequency division coefficients of the two stepping motors; four bipolar H-bridge power drive circuits are used for amplifying the pitch axis SPWM waves and the azimuth axis SPWM waves and then controlling the two stepping motors to drive the azimuth axis and the pitch axis to rotate, and a four-quadrant detector is driven to conduct scanning and tracking. According to the invention, the single-chip DSP and the single-chip FPGA are adopted to realize the subdivision driving and closed-loop control of the azimuth axis and the pitch axis based on the stepping motors, and the required control function and performance index are realized under the condition of not adding additional control chips and sensors, so that the circuit and the structure are simplified, and the requirements of space application are met.

Description

technical field [0001] The invention relates to the technical field of scanning and tracking control, in particular to a scanning and tracking control system and method for a space rendezvous and docking laser radar. Background technique [0002] In space rendezvous and docking, lidar is a major measurement device. The working principle of the laser radar is: the laser sends a single pulse laser (that is, the main wave), and the laser returns to the original path after hitting the cooperative target; the detector receives the laser echo, measures the time difference between the main wave and the echo, and calculates the target Straight-line distance to radar. According to the azimuth and elevation angles emitted by the laser, combined with the straight-line distance, the position of the target in the polar coordinate system centered on the radar is obtained. [0003] Due to the strong directivity of the laser, the divergence angle of the beam and the acceptance angle of th...

Claims

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Application Information

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IPC IPC(8): G05B19/042G01S7/481G01S17/06G01S17/42
CPCG05B19/0423G01S17/06G01S17/42G01S7/4817G05B2219/25257Y02A90/10
Inventor 周黎杨武刘恩海周向东冯志辉岳永坚袁林晨刘光林代冬军
Owner INST OF OPTICS & ELECTRONICS - CHINESE ACAD OF SCI
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