SOLUTION MANAGMET’S TASK INTEGRATED SYSTEM OF UNMANNED AIRCRAFT IN CONDITIONS OF UNCERTAINITY
DOI:
https://doi.org/10.18372/2306-1472.48.47Abstract
Abstract. In this article the methods of increase the efficiency of the compensation of indignations of theonboard integrated control systems of Unmanned Aircrafts are considered. On the basis of generalizationthe disadvantages of inertial and satellite navigation systems it was revealed, that as a result of theinsufficient compensation of indignations these systems lose a stable condition. They are exposed to barriersand there is unlimited growth of mistakes in time. For the solution of this actual problem of the onboardintegrated control systems a method of increase the efficiency of the compensation of indignations of nonstationarylinear systems in the conditions of uncertainty with the observer and with the correction bymistake of recovery was suggested. For this purpose the conditions of uncertainty were mathematicallystated, the equations of the onboard integrated control systems were completed, as non-stationary object ofmanagement, the observer with correction by mistake of recovery and a matrix of factor of strengthening ofthe observer are made. As a result the system is asymptotically stable to low-frequency indignations and theaccumulation of an error in time at high-frequency indignations is eliminated.Keywords: a condition of uncertainty, a matrix of factor of strengthening of the observer, iasymptoticalstability, low-frequency and high-frequency indignations, nertial and satellite navigation systems, nonstationarylinear systems, onboard integrated control systems, the observer with a correction by mistake ofrecovery, unmanned aircrafts.References
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