A Realization Method of Cooperative Target Control in Calibration Flight Route
A technology of cooperation goals and realization methods, applied in the direction of electrical digital data processing, transmission systems, instruments, etc., can solve problems such as waste of resources, difficulty in installation, control, and inability to change, and achieve low-cost effects
Active Publication Date: 2020-05-22
PLA NO 63686 CORPS
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Problems solved by technology
In the calibration flight of the sea-based measurement and control system, since the measurement and control equipment covers multiple frequency bands, and each frequency band has multiple working modes that need to be identified, there are many cooperation targets on the aircraft, which brings great difficulties to installation and control; especially before flight The working mode of the cooperation target is set, and it cannot be changed during the school flight route. As a result, even if a certain mode meets the data volume requirements, the mode can only be changed in the next sortie, resulting in a great waste of resources
In order to reduce the number of cooperation targets and improve the reliability of the system, when the cooperation target can achieve mode control, the original method of adding power to a single control device is no longer suitable for the needs of school flight, and it is urgent to provide a method that can According to the needs, the cooperative target mode is switched to improve flight utilization and save flight consumption
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[0028] In the mission in 2017, using the cooperative target control method in the school flight route, the accurate control of the cooperative target on the aircraft was realized, which greatly improved the utilization rate of the school flight route. In the past, at least 8 sorties were required to complete the task. It was successfully completed with only 7 sorties, making an important contribution to the school flight mission.
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The invention relates to a method for implementing cooperative target control in a calibration flight airway. The method comprises the following steps of: S1, carrying out scheme fiction on a system by adopting a hierarchical design concept, wherein a protocol conversion case is a primary control object and takes charge of distinguishing power-on power-off and mode switching instructions and distributing the power-on power-off and mode switching instructions to a power supply control case or a cooperative target, the power supply control case or the cooperative target is a secondary control object, the power supply control case completes relay control according to the instruction, and the cooperative target receives the mode switching instruction to complete mode switching; and S2, carrying out data frame design by adopting a cut-off control protocol, carrying out data frame judgment according to a data length, distinguishing a control mode according to a functional code, distinguishing a serial port number according to an address code, and sending out an object protocol frame by a designated serial port, wherein an object feedback frame is a data frame fed back by a responder or a Modbus device.
Description
technical field [0001] The invention relates to a method for realizing cooperative target control in flight calibration routes. It belongs to the technical field of control engineering. Background technique [0002] For the roadbed or sea-based measurement and control system, after the upgrade and transformation of the measurement and control equipment, etc., the regular inspection of the whole system is generally carried out by means of calibration flight technology. The so-called calibration flight is to assemble cooperative targets (transponders, etc.) on the aircraft, the aircraft will fly according to the predetermined flight path, the measurement and control equipment will track the targets on the aircraft, and the on-board accuracy identification and tracking parameters of the measurement and control system will be processed to complete the performance inspection or accuracy analysis. Thereby improving the orbit determination accuracy in the task. In the calibration...
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IPC IPC(8): H04L29/06G06F13/42
CPCG06F13/4286H04L69/08
Inventor 谢勇潘高峰瞿元新何剑伟夏利利刘四方
Owner PLA NO 63686 CORPS
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