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Combination missile target imitation flight test system

A test system and combined technology, applied in the direction of electrical testing/monitoring, can solve the problems of high operation cost, high cost, single function, etc., and achieve the effect of simple structure, low cost and high efficiency

Active Publication Date: 2014-04-23
HUBEI SANJIANG AEROSPACE HONGFENG CONTROL
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The traditional hardware-in-the-loop simulation system is mainly used for attitude control, its function is relatively single, and its cost is high, and its operating cost is high, so it is not suitable for the combined target missile control system. Therefore, it is urgent to develop a combination target missile Fly-like test system, which not only realizes the pertinence of control system simulation, but also is easy to operate, flexible in development mode, and high in operating efficiency

Method used

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  • Combination missile target imitation flight test system
  • Combination missile target imitation flight test system
  • Combination missile target imitation flight test system

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Experimental program
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Effect test

Embodiment approach

[0040] According to an embodiment of the present invention, the simulation development machine specifically includes:

[0041] The flight control model building block is used to establish the kinematics and dynamics model of the combined target missile. Based on the kinematics and dynamics model of the combined target missile, two types of target based on virtual rudder and simulated rudder are constructed. Missile flight control model;

[0042] The model running module is used to simulate and run the target missile flight control model offline, record the rudder control signal during the running process in real time, and send it to the human-machine interaction module;

[0043] The human-computer interaction module is used to provide a human-computer interaction interface to realize the monitoring of the simulation flight test process, and compare the rudder control signal recorded by the model running module with the rudder control signal fed back by the simulation test host...

example

[0061] NI real-time embedded controller PXI-8109RT, with Intel i7-620M dual-core processor, maximum memory 4GB DDR3-1066MHz, 120GB hard disk, 4 high-speed USB ports, 1 RS232 interface; equipped with USB interface, network port and keyboard / mouse , display interface, etc., the Windows XP operating system and LabVIEW RT real-time operating system attached to NI are pre-installed, as well as the drivers of various modules;

[0062] DA board: NI PXI-67338 channels, 16 bits, 250ks / s; 8 analog D / A output channels, resolution 16 bits, maximum update rate 1MS / s, output voltage range 0~±10V; digital I / A 8 O channels; 2 24-bit counters;

[0063] AD board: NI PXI-6251 analog signal differential acquisition channel 8 channels, resolution 16 bits, maximum sampling rate 1.25±MS / s (programmable), maximum input voltage ±10V; analog signal output channel 2 channels, resolution The rate is 16 bits, the maximum update rate is 2.8MS / s, the maximum output voltage is ±10V; digital I / O channels are...

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Abstract

The present invention discloses a combination missile target imitation flight test system, which includes a simulation development machine used in building a combination missile target flight control model, translating the simulation development machine into an executable code; an off-line simulation operation control model which records a rudder control signal and receives the rudder control signal from a simulation test host, comparing with the rudder control signal of the simulation operation model to judge the accuracy of a flight control software of the control system or the operation of a steering gear; the simulation test host which executes the executable code, sends the relevant track information of executing output to an interface box and sends the rudder control signal of an on-board control system transferred by the interface box to the simulation development machine; the interface box which is used for transferring the signals between the simulation test host and the on-board control system. The combination missile target imitation flight test system can perform a simulation test and a simulation experiment for the flight control system of multi-module and complex logic from model modification to physical simulation once, and is characterized by simple framework, low cost and high efficiency.

Description

technical field [0001] The invention belongs to the technical field of flight control and simulation, and in particular relates to a combined target missile flight imitation test system, which is used for performing simulation tests and simulation tests on a multi-module and complex logic target missile flight control system. Background technique [0002] With the development of technology and the application needs of diversified functions, the design of the target missile control system for simulating high-speed moving targets tends to be combined and serialized. The combined target missile control system has the characteristics of multi-module, combined, and complex logic. The traditional hardware-in-the-loop simulation system is mainly used for attitude control, its function is relatively single, and its cost is high, and its operating cost is high, so it is not suitable for the combined target missile control system. Therefore, it is urgent to develop a combination target...

Claims

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Application Information

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IPC IPC(8): G05B23/02
Inventor 张朝阳佘君陈公仆
Owner HUBEI SANJIANG AEROSPACE HONGFENG CONTROL
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