Digital aircraft attitude and orbit control component combination distribution source code artificial intelligence writing method
A component combination and artificial intelligence technology, applied in attitude control, instruments, control/regulation systems, etc., can solve the problems of time-consuming and labor-intensive, reduce code readability and maintainability, and achieve the effect of reducing simulation costs
Active Publication Date: 2020-05-19
BEIHANG UNIV
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Problems solved by technology
At present, it is basically relying on human beings to ensure the consistency of the data transmission content and format in the digital aircraft simulation code, which is time-consuming and laborious, and it is difficult to form a relatively stable and standardized data transmission format in the same simulation program, which reduces the readability and readability of the code. maintainability
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[0035] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.
[0036] The invention provides a method for writing artificial intelligence source codes for the combined distribution of digital aircraft attitude and orbit control components. For issues such as the compilation of components and the data connection relationship in the combination and allocation of attitude and orbit control components, the source code of the combination of components can be intelligently written according to the aircraft structure design resul...
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The invention provides an artificial intelligence writing method for combination distribution source codes of digital aircraft attitude and orbit control components. Digital aircraft attitude and orbit control components each comprise a sensor and an executing mechanism. On the base of component mounting information and component model codes, artificial intelligence substitutes people to write physical quantity input functions, initialization functions, state quantity refreshing functions and physical effect calculation functions of digital aircraft attitude and orbit control component combinations, and intelligent writing of the attitude and orbit control component combination source codes in an aircraft closed-loop control system is achieved. According to the artificial intelligence writing method, artificial intelligence is used for substituting people, the source codes of the attitude and orbit control component combinations in a whole set of digital aircraft simulation program arewritten intelligently according to the model code and the installation mode of one single digital aircraft attitude and orbit control component, the writing efficiency is improved, and the aircraft simulation cost is lowered.
Description
technical field [0001] The invention relates to the field of aircraft design, and more specifically relates to an artificial intelligence writing method for combining and distributing source codes of digital aircraft attitude and orbit control components. Background technique [0002] In the process of aircraft design and development, in order to ensure the high reliability of the final application of the aircraft, it is necessary to adopt a large number of existing design mainstream methods in the design, and it is necessary to conduct simulation verification and ground tests. Among them, some ground tests cannot fully reflect the actual working conditions of the aircraft in orbit, and the cost is high, so it is limited. [0003] Digital aircraft simulation verification is not limited by environmental conditions, and as long as the model is established accurately enough, the working conditions of the aircraft can be better simulated. Therefore, simulation verification metho...
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IPC IPC(8): G05D1/08G05D1/10
CPCG05D1/0808G05D1/101
Inventor 董云峰李培昀赵欣博
Owner BEIHANG UNIV