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A Compensation Simulation Method for Turntable Applicable to Simulating Projectile Attitude Motion

A simulation method and compensation technology, applied in the field of guided weapon simulation, can solve problems such as the mechanical angle limit of the turntable

Active Publication Date: 2022-04-29
西安现代控制技术研究所
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  • Claims
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Problems solved by technology

[0010] In order to solve the above problems, the present invention provides a compensating simulation method for a turntable suitable for simulating the posture movement of a projectile body, which solves the problem of the mechanical angle limit of the turntable caused by an excessively large negative pitch angle, and can meet the requirements of large drop angle attacks. Patterned weapon system hardware-in-the-loop simulation requirements

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  • A Compensation Simulation Method for Turntable Applicable to Simulating Projectile Attitude Motion
  • A Compensation Simulation Method for Turntable Applicable to Simulating Projectile Attitude Motion
  • A Compensation Simulation Method for Turntable Applicable to Simulating Projectile Attitude Motion

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Embodiment Construction

[0028] In order to enable those skilled in the art to better understand the solutions of the present application, the technical solutions in the embodiments of the present application will be clearly and completely described below in conjunction with the drawings in the embodiments of the present application.

[0029] Such as figure 1 As shown in , under the condition that the mechanical angle of the turntable is limited, a compensation simulation method for the turntable that is suitable for simulating the attitude motion of the missile body includes the following steps:

[0030] S1: Give the turntable an initial yaw angle ψ' 0 , initial roll angle γ' 0 and the initial pitch angle θ′ 0 , and is the initial pitch angle θ′ 0 superimposed a constant sacrificial angle Δ xs ;

[0031] S2: The simulation computer calculates the attitude angle, and then calculates the yaw angle ψ' fzj , roll angle γ' fzj and superimposed on the sacrificial angle Δ xs pitch angle θ′ zt send ...

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Abstract

The invention provides a compensating simulation method for a turntable suitable for simulating the attitude motion of a projectile. By superimposing the sacrificial angle and the compensation angle method, on the premise of sacrificing the active range of the turntable's positive pitch angle, it solves the problems caused by the negative pitch angle. The problem of the mechanical angle limit of the turntable caused by too large angle meets the requirements of the hardware-in-the-loop simulation of the weapon system in the large-fall angle attack mode, realizes the closed-loop experiment of the weapon system hardware-in-the-loop simulation in the large-fall angle attack mode, and provides a basis for the weapon development of the guided rocket project Provided a strong guarantee.

Description

technical field [0001] The invention belongs to the technical field of guided weapon simulation, and in particular relates to a compensating simulation method for a turntable suitable for simulating the attitude motion of a missile body. Background technique [0002] The turntable has the function of simulating the attitude movement of the projectile body, and is an indispensable part of the test equipment for the semi-physical simulation test of the guided weapon system. The vertical turntable is a type of turntable divided according to the form of mechanical structure, which meets the omnidirectional launch requirements of the rocket-guided weapon system. [0003] Traditional hardware-in-the-loop simulation methods for weapon systems include the following steps: [0004] S1: Fix the inertial navigation device on the vertical turntable, and bind the initial projectile attitude information (θ 0 、ψ 0 , γ 0 ), initialize the attitude angle of the turntable, and wait for th...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F42B35/00G06F30/20G06F119/14
CPCF42B35/00
Inventor 刘梦焱刘琦刘满国肖堃王娇张翔朱克炜王鹏高晓波娄江方莉邓海鹏王博李昊梁益铭党元杰范中平
Owner 西安现代控制技术研究所
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