Aircraft guidance control simulation test method and device

Abstract

The embodiment of the application provides an aircraft guidance control simulation test method and device. The method comprises the steps: respectively building subsystem models of all controlled objects corresponding to a preset guidance control system model of an aircraft based on historical simulation engineering data of the aircraft; establishing a guidance control simulation system of the aircraft in a virtual simulation environment according to the guidance control system model of the aircraft and each subsystem model; performing simulation verification on the operation state of the guidance control simulation system so as to debug operation parameters of the guidance control simulation system according to a simulation verification result; and accessing preset hardware equipment intothe guidance control simulation system to carry out a semi-physical simulation test for the aircraft. According to the application, the integrated simulation test between the guidance control systemand the controlled subsystem of the aircraft can be effectively realized, and the accuracy and reliability of the aircraft guidance control simulation test can be improved by providing an open and extensible virtual integrated simulation and test environment.

Description

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AI Technical Summary

Benefits of technology

This patented describes how flight simulator systems are designed with software modules called guided controls or computerized controllers. These simulations allow pilots to train their skills beforehand during training without actually flying them down on airplanes. They also have access through communication networks like LAN connections, allowing remote monitoring over longer distances while still being able to operate safely within restricted areas around the world's borders. Overall, this approach allows pilots more efficient ways to plan and execute mission plans than current methods based only on physical experimentations.

Problems solved by technology

The technical problem addressed in this patented text relates to improving the accuracy and reliability of simulating an airborne guiding/controlled object during flight simulations on real world objects such as manned drones. This requires developing models from which pilot controls are able to interact more accurately than current methods without sacrificing safety concerns associated therewith.

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