Optical cooperative orbit determination method for small celestial body surrounding detector

A technology for detectors and small celestial bodies, applied in the field of deep space exploration, can solve problems such as limiting the accuracy of optical orbit determination, terrain database errors, and increasing the technical difficulty of tasks, so as to improve the accuracy of optical orbit determination and simplify the technical difficulty.

Active Publication Date: 2020-01-14
BEIJING INSTITUTE OF TECHNOLOGYGY
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Problems solved by technology

However, this method requires obtaining the terrain database of small celestial bodies in advance, which greatly increases the technical difficulty of the task, and the terrain database itself has errors, which limits the accuracy of optical orbit determination.

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  • Optical cooperative orbit determination method for small celestial body surrounding detector
  • Optical cooperative orbit determination method for small celestial body surrounding detector
  • Optical cooperative orbit determination method for small celestial body surrounding detector

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Embodiment Construction

[0035] In order to better illustrate the purpose and advantages of the present invention, the content of the invention will be further described below in conjunction with the accompanying drawings and embodiments.

[0036] Such as figure 1 As shown, this example focuses on the optical cooperative orbit determination method for small celestial bodies around the detector, and the specific implementation method is as follows:

[0037] Step 1: Consider the position and velocity vectors of the two detectors as state variables to be estimated, and establish a state model for optical cooperative orbit determination in the small celestial body fixed coordinate system.

[0038] The positions and velocities of the two detectors are shown in formula (1).

[0039] X=[r 1 ,v 1 ,r 2 ,v 2 ] T (1)

[0040] The state model of optical cooperative orbit determination is established in the fixed coordinate system of small celestial bodies, as shown in formula (2).

[0041]

[0042] wh...

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Abstract

The invention discloses an optical cooperative orbit determination method for a small celestial body surrounding detector, and belongs to the technical field of deep space detection. The method comprises the steps: taking the positions and speed vectors of two detectors as to-be-estimated state variables, and establishing an optical collaborative orbit determination state model under a small celestial body fixed connection coordinate system; imaging the observed detector through a camera of the observation detector to obtain pixel information of the observed detector in a phase plane, and establishing an observation model of optical collaborative orbit determination in combination with the known attitude of the observation detector; employing a nonlinear navigation filtering algorithm to carry out cooperative estimation on the positions and the speed vectors of the two detectors, and achieving the optical cooperative orbit determination of the small celestial body surrounding the detectors. The method comprises but is not limited to two detectors; when multiple detectors are arranged, relevant detection attributes are given to the detectors according to the actual small celestial body surrounding detector optical collaborative orbit determination requirement, and small celestial body surrounding detector optical collaborative orbit determination is achieved by observing opticalmeasurement between the detectors and the observed detector.

Description

technical field [0001] The invention relates to an optical cooperative orbit determination method for a small celestial body surrounding a detector, and belongs to the technical field of deep space detection. Background technique [0002] The orbit determination of small celestial bodies around the detector is of great significance for the design of motion orbits near small celestial bodies, scientific observation of small celestial bodies, and safe landing sampling of small celestial bodies. It is one of the key technologies in small celestial body detection missions. Optical observation is a commonly used orbit determination technology for small celestial bodies orbiting detectors. In previous missions, the orbiting detectors optically imaged the surface of small celestial bodies to obtain surface topographic feature points, and then matched the feature points with the prior terrain database to achieve optical orbit determination. However, this method requires the terrain...

Claims

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Application Information

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IPC IPC(8): G01C21/24
CPCG01C21/24
Inventor 秦同乔栋黄江川刘梓萱
Owner BEIJING INSTITUTE OF TECHNOLOGYGY
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