Dynamic power balance analyzing system for lunar explorer

Abstract

The invention relates to a dynamic power balance analyzing system for a lunar explorer and belongs to the technical field of lunar explorers. According to the dynamic power balance analyzing system disclosed by the invention, the energy analyzing process of the whole process from the emulation start to emulation ending is realized, relevant information conditions of power balance in the whole flying process are dynamically displayed and the omni-bearing power balance information is presented by using various modes such as a process curve, graph display and digital list display. The dynamic power balance analyzing system has a function of modifying flying programs; users can be allowed to simply input new flying programs; and the adaptability of different programs is solved. According to the dynamic power balance analyzing system disclosed by the invention, a system model library is established; parameters of the system model library are outputted to fit actual telemetry parameters of an aircraft and an analysis result with higher accuracy is obtained.

Description

technical field [0001] The invention relates to a dynamic power balance analysis system of a lunar exploration aircraft, and belongs to the technical field of lunar exploration aircraft. Background technique [0002] Lunar exploration vehicles have relatively strict weight requirements and unstable lighting conditions. During the flight, they often need to perform orbital change maneuvers many times, resulting in a relatively tight energy situation for the vehicle. Therefore, the dynamic display and prediction of the energy flow during the flight of the aircraft is urgently required. In this case, the previous manual calculations cannot meet the requirements of the overall design and development of the aircraft. [0003] Therefore, it is very necessary to develop a dynamic power balance analysis system for lunar exploration vehicles that is suitable for calculation of complex operating modes. Contents of the invention [0004] The purpose of the present invention is to pr...

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Problems solved by technology

[0002] Lunar exploration vehicles have strict weight requirements and unstable lighting conditions. During the flight, they often need to perform orbital maneuvers many times, resulting in a relatively tight energy situation for the vehicle.

Therefore, the dynamic display and prediction of the energy flow during the flight of the aircraft is urgently required. In this case, the previous manual calculations cannot meet the requirements of the overall design and development of the aircraft.

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