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A study of the responsiveness to precision of measurements of algorithm of the trajectory control under self-guidance of aerial vehicles on high-speed aircraft

Keywords:

V.I. Merkulov, D.A. Milyakov


Tactical advantages of high-speed, highly-maneuverable aircraft are shown. This type of aircraft usage predetermines the development of new all-aspect guidance methods. One possible alternative algorithm of all-aspect guidance of aerial vehicle on high-speed, highly-maneuverable aircraft is proposed. Detailed study of the algorithm’s responsiveness to precision of measurements of various phase coordinates in various application conditions is carried out. Based on results of the study, the algorithm application recommendations are presented.
References:
  1. Merkulov V. I., Drogalin V. V., Kanashhenkov A. I. i dr. Aviacionnye sistemy radioupravlenija. T. 2. Radioehlektronnye sistemy samonavedenija / Pod red. A. I. Ka-nashhenkova i V. I. Merkulova. M. : Radiotekhnika. 2003. 392 s.
  2. Kanashhenkov A. I., Merkulov V. I., Samarin O. F. Oblik perspektivnykh bortovykh radiolokacionnykh sistem. Vozmozhnosti i ogranichenija. M.: IPRZHR. 2002.
  3. Patent RF na izobretenie № 2408847.
  4. Merkulov V. I., Drogalin V. V, Kanashhenkov A. I. i dr.Aviacionnye sistemy radioupravlenija. T. 1. Principy postroenija sistem radioupravlenija. Osnovy sinteza i analiza / Pod red. A. I. Kanashhenkova i V. I. Merkulova. M.: Radiotekhnika. 2003. 192 s.
June 24, 2020
May 29, 2020

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