High-precision and high-efficiency aircraft trajectory optimization and guidance switching method and system

A trajectory optimization and switching system technology, applied in the field of aircraft, can solve the problems of errors and low accuracy of aircraft, and achieve the effects of improving accuracy, improving obstacle avoidance efficiency, and ensuring high accuracy and high agility

Pending Publication Date: 2021-10-01
中国人民解放军火箭军工程大学
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  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Through the above analysis, the problems and defects of the existing technology are: the accuracy of trajectory optimizati...

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  • High-precision and high-efficiency aircraft trajectory optimization and guidance switching method and system

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Embodiment Construction

[0053] In order to make the object, technical solution and advantages of the present invention more clear, the present invention will be further described in detail below in conjunction with the examples. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0054] Aiming at the problems existing in the prior art, the present invention provides a high-precision and high-efficiency aircraft trajectory optimization and guidance switching method and system. The present invention will be described in detail below with reference to the accompanying drawings.

[0055] Such as figure 1 As shown, the high-precision and high-efficiency aircraft trajectory optimization and guidance switching system provided by the embodiment of the present invention includes: a data acquisition module 1, a data preprocessing module 2, a central control module 3, an optimization area definition module 4, ...

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Abstract

The invention belongs to the technical field of aircrafts, and discloses a high-precision and high-efficiency aircraft trajectory optimization and guidance switching method and system. The high-precision and high-efficiency aircraft trajectory optimization and guidance switching system comprises a data acquisition module, a data preprocessing module, a central control module, an optimization area defining module, a trajectory optimization model building module, an initialization module, a trajectory optimization module, a guidance switching module, a data storage module and an update display module. According to the invention, the trajectory optimization module utilizes the high-precision and high-efficiency aircraft trajectory optimization model to realize optimization processing of the aircraft trajectory, so that the precision of high-precision and high-efficiency aircraft trajectory optimization is improved, and high accuracy and high agility of a high-precision and high-efficiency aircraft precise strike task are ensured. Meanwhile, a multi-mode switching guidance law conforming to the current flight environment situation is formed through a guidance switching module by adopting a nonlinear model prediction control method, and the obstacle avoidance efficiency of the high-precision and high-efficiency aircraft is improved.

Description

technical field [0001] The invention belongs to the technical field of aircraft, and in particular relates to a high-precision and high-efficiency aircraft trajectory optimization and guidance switching method and system. Background technique [0002] At present, aircraft can achieve global rapid and precise strikes and reach missions, and its related technologies have attracted extensive attention from global military powers, and have become an extremely important development direction in the world's aerospace field. With its extremely high flight speed and long-span flight distance, aircraft has very important significance in military strategy, and is increasingly valued by countries all over the world. [0003] In the study of aircraft, trajectory optimization and tracking guidance is a significant topic, especially complex flight missions require the aircraft to have the ability to plan trajectory autonomously. The trajectory optimization of the re-entry segment of the ...

Claims

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Application Information

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IPC IPC(8): G05D1/10
CPCG05D1/101Y02T10/40
Inventor 蔡光斌徐慧李欣肖永强杨小冈杨波席建祥
Owner 中国人民解放军火箭军工程大学
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