Solid-liquid power cruising aircraft flight mission planning simulation system

Abstract

The invention discloses a solid-liquid power cruising aircraft flight mission planning simulation system which is composed of a user operation interface, an aircraft simulation model and a graphic data processing module. The user operation interface is mainly used for human-computer interaction, flight scheme design and flight data analysis. The aircraft simulation model is mainly used for backstage operation and design scheme implementation. The graphic data processing module is mainly used for completing data storage and graphic display after simulation is over. The solid-liquid power cruising aircraft flight mission planning simulation system mainly has the following functions: the first function is scheme trajectory planning to obtain the cruising height, cruising time and cruising speed of various flight schemes; the second function is to complete control scheme planning and parameter setting to select different control schemes; the third function is to complete simulation data storage and analysis and ballistic trajectory display. The solid-liquid power cruising aircraft flight mission planning simulation system realizes integrated design and fusion of a cruising aircraft trajectory scheme, a control scheme and simulation data and realizes simulation and verification of a total design scheme according to the characteristics of a solid-liquid power cruising aircraft.

Description

technical field [0001] The invention belongs to the field of flight simulation, and in particular relates to a novel flight task planning simulation system for a cruise aircraft with solid-liquid power. Background technique [0002] The solid-liquid powered cruising aircraft is a new type of cruising aircraft, which uses a solid-liquid rocket engine as a power device. The solid-liquid rocket engine has high safety and good economy, and compared with the solid rocket engine, it can realize thrust adjustment and long-term work. The rocket engine has a simple structure and is easy to use. From the perspective of technology, safety and economy, the solid-liquid rocket engine has great advantages in the development of a new generation of cruise power system. During the flight, the variable thrust control of the aircraft can be realized by adjusting the flow rate of the liquid oxidant and changing the combustion rate of the propellant; mathematical simulation is an indispensable l...

AI Technical Summary

Problems solved by technology

In the design process of new aircraft, it is necessary to continuously verify the calculation data, change the design scheme and feed back the simulation data. Such tedious and redundant work is not only a waste of time, but also prone to errors

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