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Control method of Risley prism system applied to airborne infrared aided navigation

A technology for assisting navigation and control methods, which is applied in the field of servo control and can solve the problems of inaccurate control algorithm of Risley prism beam pointing and unclear rotation control model of biprism.

Active Publication Date: 2016-09-21
西安应用光学研究所
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Problems solved by technology

[0007] Aiming at the problems in the prior art that the dual prism rotation control model is unclear and the Risley prism beam pointing control algorithm is inaccurate, etc., the invention uses a reverse accurate analytical algorithm based on the non-paraxial vector ray tracing method to propose a method that can accurately realize The Risley prism system rotation control model o

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  • Control method of Risley prism system applied to airborne infrared aided navigation
  • Control method of Risley prism system applied to airborne infrared aided navigation
  • Control method of Risley prism system applied to airborne infrared aided navigation

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Embodiment Construction

[0054] The present invention will be further described in detail below in conjunction with the example of line-of-sight pointing scanning simulation and corresponding drawings.

[0055] At first narrate basic principle of the present invention:

[0056] 1. Risley Prism System Reverse Accurate Analytical Algorithm

[0057] The Risley prism system deflects the incident light so as to change the direction of light propagation. The airborne infrared auxiliary navigation equipment uses the relative rotation of the double prism to guide the outgoing beam to the preset direction, and realizes the direction of the line of sight through reverse accurate analytical calculation. The required rotation angle of the double prism realizes the scanning movement of the line of sight.

[0058] 1) Line of sight pointing vector transformation

[0059] During the working process of the airborne infrared auxiliary navigation equipment, the line of sight points to continuously move to form a conti...

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Abstract

The invention provides a control method of Risley prism system applied to airborne infrared aided navigation. The method comprises the following steps: using sight lines to point to vector commands as input, using the reverse exact analysis algorithm based on the non-paraxial vector ray tracing algorithm, calculating the rotation angles of the prism which can accurately realize the pointing requirement of the sight lines, and using them as control model outputs. This method can effectively solve the problem in practical use that the rotation angles of the prism are on constant large expansion due to the continuous sight line scanning and the mutually independent calculation processes for the rotation angles of the prism corresponding to the vectors pointed to by scattered sight lines, therefore improving the stability and efficiency of prism rotation. The simulation and the implementation results show that the control method can achieve the aim of the invention, has the advantages of precise control of the pointing of sight lines and good control effect for prism rotation. At the same time, as a software control algorithm, the method is cost-effective and can be promoted for wider applications.

Description

technical field [0001] The invention belongs to the field of servo control of aiming line pointing in airborne infrared auxiliary navigation equipment, and mainly relates to a precise control model of a Risley prism system, specifically a control method for a Risley prism system applied to airborne infrared auxiliary navigation, ensuring that the prism Continuous, smooth, efficient rotation. Background technique [0002] The airborne infrared auxiliary navigation equipment is used for the aircraft to scan and observe the area ahead of the flight route at night or under complex weather conditions, and form a clear geographical image in real time for the pilot to observe, which can improve the pilot's perception of the air-ground situation and improve the night vision of the aircraft combat capability. [0003] At present, many airborne infrared auxiliary navigation devices have changed from the traditional form of hanging photoelectric pods to the form of integration with th...

Claims

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Application Information

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IPC IPC(8): G05D1/08G02B26/08
CPCG02B26/08G05D1/0808
Inventor 王宏浩贠平平陶忠韩梅舒营恩别勇军卢晓敏张晶
Owner 西安应用光学研究所
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