Flight simulation test system for solid-liquid power aircraft

A flight simulation and test system technology, applied in the field of control systems, can solve the problems that the operability and intelligence cannot reflect the level of mathematical simulation, the process of error checking is difficult, and resources are occupied, so as to shorten the development cycle and simplify the composition and design process , Improve the effect of simulation time

Inactive Publication Date: 2014-08-27
BEIHANG UNIV
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Problems solved by technology

However, such tedious and redundant work occupies most of the resources of the system, and the operation is complicated. If there is a problem in any intermediate simulation link, the process of troubleshooting is also very difficult; at the same time, a simulation system separates data processing, display, and calculation. Its operability and intelligence cannot reflect the current level of mathematical simulation

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  • Flight simulation test system for solid-liquid power aircraft
  • Flight simulation test system for solid-liquid power aircraft
  • Flight simulation test system for solid-liquid power aircraft

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Embodiment Construction

[0035] The present invention will be further described below in conjunction with the accompanying drawings.

[0036] A kind of solid-liquid power aircraft flight simulation test system proposed by the present invention, such as figure 1As shown, it includes an aircraft simulation model system 1, an integrated console system 2, and a data processing system 3. Wherein, the integrated console system 2 is the entrance of the simulation program, the aircraft simulation model system 1 is the core of the simulation program, and the data processing system 3 and the aircraft simulation model system 1 run in the background of the program.

[0037] The aircraft simulation model system 1 is to complete the corresponding module functions by the class written based on C++, which mainly includes a quality module 101, a flight environment module 102, an integrated navigation module 103, a timing control module 104, an aircraft model module 105, a control system module 106, A power system mod...

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Abstract

The invention discloses a flight simulation test system for a solid-liquid power aircraft. The flight simulation test system for the solid-liquid power aircraft comprises an integrated console system, an aircraft simulation model system and a data processing system. The integrated console system is mainly used for setting system parameters, monitoring key variables and status information, starting and controlling programs, checking operation instructions and the like. The aircraft simulation model system is mainly used for conducting operation calculation of each system model. The data processing system is mainly used for achieving the simulation data processing function and the simulation data storage function. According to the characteristics of the solid-liquid power aircraft, the flight simulation test system mainly achieves the following functions that firstly, simulation ballistic trajectories can be set according to the task requirements; then, diversification control rate can be set and an efficiency test can be conducted; finally, the real-time monitoring function and the storage function of the status of the system can be achieved.

Description

technical field [0001] The invention belongs to the field of control systems, and in particular relates to a novel flight simulation test system for a solid-liquid powered aircraft. Background technique [0002] The solid-liquid powered aircraft is a new type of aircraft that uses a solid-liquid hybrid engine as a power device, has the characteristics of repeatable start, adjustable thrust, etc., and has high safety and good economy. Compared with liquid-powered engines, it is easy to operate and has a simple structure. Compared with solid-powered engines, it can work for a long time and the thrust can be adjusted. The working principle of the engine is that after the igniter is triggered, the liquid valve is opened to release the liquid oxidant. The oxidant contacts and burns with the solid fuel in the combustion chamber, and the engine starts to work. At the same time, the booster valve is opened to adjust the oxidant flow rate and change the combustion rate of the propell...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B17/02
Inventor 宋佳蔡国飙李小川王鹏施文杰
Owner BEIHANG UNIV
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