In the process of using airborne flight navigation complexes (AFNCs) for their intended purpose, a change in the operating conditions or the failure of its elements leads to various consequences, depending on the structure of the complex or the class of tasks being solved. Firstly, a change in the operating conditions (failure of individual elements of the complex) leads to a sharp decrease in the efficiency of solving flight and navigation tasks. At the same time, the AFNC as a whole can exist in one of two states: operable or failure. However, this model is typical only for particular problems. Secondly, the AFNC is reconfigured when the operating conditions change. This allows to temporary solve flight and navigation tasks with acceptable, albeit lower quality. This is the most typical situation for navigation tasks. Both in the first and in the second cases, the technical condition monitoring algorithms of the AFNC should inform the user about the violation of the operating conditions within a specified time with required detection and false alarm probabilities. The paper presents a technique for determining the operability scope of an airborne flight navigation complex on a set of invariant control ratios, which allows development of optimal control algorithms.
The Technique of Determining the Operability Scope of an Airborne Flight Navigation Complex on a Set of Invariant Control Ratios
Lect.Notes Mechanical Engineering
Proceedings of 10th International Conference on Recent Advances in Civil Aviation ; Chapter : 16 ; 179-187
2022-10-20
9 pages
Article/Chapter (Book)
Electronic Resource
English
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