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Flight control simulation system with fault diagnosis capability for unmanned helicopter

An unmanned helicopter and simulation system technology, applied in the field of UAV flight control system design, can solve the problems that the simulation environment is not seen, the flight control system simulation environment is rarely seen, etc., and achieves the effect of a high degree of replacement

Inactive Publication Date: 2017-02-22
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

It is rare to see a flight control system simulation environment with fault diagnosis capabilities, especially for an unmanned helicopter flight control system simulation environment with fault diagnosis capabilities

Method used

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  • Flight control simulation system with fault diagnosis capability for unmanned helicopter
  • Flight control simulation system with fault diagnosis capability for unmanned helicopter
  • Flight control simulation system with fault diagnosis capability for unmanned helicopter

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Experimental program
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Embodiment Construction

[0051] The present invention has the flight control simulation system of the unmanned helicopter of fault diagnosis capability, such as figure 1 As shown, the system is composed of a simulation master console, a simulation computer, a flight control management system, a sensor system, a physical effect device, a servo system, a remote control telemetry system, and a mission load system; the relationship between them is as follows: the simulation master control Station control simulation computer start-up detection, model generation and injection of fault models, simulation main console control flight control management system start-up detection and real-time detection of the working status of the flight control management system, simulation main console control physical effect equipment start-up detection, set flight task and flight conditions and generate various flight interference conditions; the simulation computer selects the simulation model, interference model and virtua...

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Abstract

The invention provides a flight control simulation system with fault diagnosis capability for an unmanned helicopter. The flight control simulation system with fault diagnosis capability for an unmanned helicopter comprises a simulation general control console, a simulation computer, a flight control management system, a sensor system, physical effect equipment, a servo system, a remote control and remote measurement system, and a task load system, wherein the simulation general control console controls the simulation computer to carry on a power on test, model generation and injection of fault model; the simulation computer selects simulation and interference model and simulates fault injection to carry on flight simulation; the flight control management system receives the information of sensors and the remote control and remote measurement system; the servo system realizes the real reaction of an operating mechanism; and the sensor system transmits the acquired sensor information to the flight control management system. For the flight control simulation system with fault diagnosis capability for an unmanned helicopter, the simulation computer can be embedded into different aircraft mathematical models, so that simulation of a plurality of aircrafts can be realized. For the flight control simulation system with fault diagnosis capability for an unmanned helicopter, the servo system and the sensor system can access a real steering engine of aircraft and real sensors so as to develop the steering engine of aircraft, to make a test flight for the steering engine of aircraft, and detecting working of the sensors.

Description

[0001] 1. Technical field [0002] The invention provides a flight control simulation system of an unmanned helicopter with fault diagnosis capability, which relates to a simulation environment, in particular to a flight control system simulation of an unmanned helicopter with fault diagnosis capability, and belongs to the design field of unmanned aerial vehicle flight control systems. [0003] 2. Background technology [0004] The flight control system is the core of the UAV system. In order to design a complete and reliable UAV flight control system, a complete and powerful simulation system can provide a strong guarantee. With the rapid development of UAVs, UAV systems are becoming more and more complex, and the requirements for UAV flight control systems are also getting higher and higher. The previous UAV flight control system basically only needs to realize the controllable flight parameters. Modern flight control systems focus on system management and intelligence, req...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B17/02B64F5/00
CPCG05B17/02
Inventor 王吉东王立新
Owner BEIHANG UNIV
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