An antenna automatic guidance method for aerospace measurement and control equipment

Abstract

The invention relates to the field of celestial servos, and more specifically, relates to an automatic antenna guidance method for aerospace measurement and control equipment. The present invention programs all the original guidance methods of the measurement and control equipment to form an automatic antenna guidance method; among them, by setting the guidance priority for different guidance methods, it is ensured that when a certain guidance method fails or recovers, the device can automatically switch to More priority guidance methods; by setting switching thresholds for different guidance methods, the correctness of the guidance methods can be judged before switching to the standby guidance method or restoring the priority guidance method, and soft switching of the guidance methods is realized; through one or more The tracking duration can be set for each guidance method, which realizes the function that the device can automatically call different guidance methods in different tracking time intervals. The invention can automatically guide the antenna to track the target without manual intervention, and greatly improves the automatic operation capability of the equipment.

Description

technical field

[0001] The invention relates to the field of celestial servos, and more specifically, relates to an automatic antenna guidance method for aerospace measurement and control equipment. Background technique

[0002] At present, when the existing aerospace measurement and control equipment guides the antenna to track the target, the operator usually manually switches between self-tracking, digital guidance, theoretical ballistic guidance, and manual guidance. When there are abnormal situations such as large data jumps and interruptions in the guidance mode, the operator needs to manually switch to other backup guidance modes, and the operator manually switches back after the abnormal guidance mode is restored. Some self-tracking methods have a backup boot function. When self-tracking fails, they can switch to the backup boot mode. However, since the switching mode is a hard switch, it is impossible to judge the correctness of the backup boot mode at that time; I...

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