Certificate of Registration Media number Эл #ФС77-53688 of 17 April 2013. ISSN 2308-6033. DOI 10.18698/2308-6033
  • Русский
  • Английский

Assessment of impact of information and ballistic launch support factors on mission realizability by aircraft formations

Published: 14.10.2021

Authors: Zakharov V.N., Kazakov G.V., Kotyashev N.N.

Published in issue: #10(118)/2021

DOI: 10.18698/2308-6033-2021-10-2121

Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control

Sensitivity plays an important role in the analysis and synthesis of technical systems no matter what complexity or purpose, that is in assessing their accuracy, determining and selecting tolerances for their parameters, or in any optimization process. One of the most important objectives of the information and ballistic launch support, along with the provision of launch data, is to increase the efficiency of aircraft in performing their missions. Therefore, it is of high relevance to assess the function of sensitivity and the function of influence of the information and ballistic launch support on the effectiveness of the functional performance of aircraft formations and ensure, at acceptable costs, the fullest use of their structural and ballistic capabilities. In this paper, we defined and evaluated functions of sensitivity and functions of influence of the main factors of information and ballistic launch support of aircraft launches on their functional performance as a formation. The degree of influence of information and ballistic support factors on the realizability of missions by aircraft formations is represented by numerical indicators. An integral indicator for assessing the impact of information and ballistic support factors on the performance indicators of aircraft formations has been formed as a weighted convolution of increments of partial indicators.

[1] Rosenwasser E.N., Yusupov R.M. Chuvstvitelnost sistem upravleniya [Sensitivity of control systems]. Moscow, Nauka Publ., 1981, 464 p.
[2] Glukhov A.P., Kotyashev N.N., Kuptsov A.V. Strategicheskaya stabilnost — Strategic stability, 2007, no. 1, pp. 39–44.
[3] Volkov E.B., Norenko A.Yu. Raketnoe protivostoyanie [Missile confrontation]. Moscow, SIP RIA Publ., 2002, 167 p.
[4] Kotyashev N.N., Lebedev P.F. Dvoнnye tekhnologii — Dual technologies, 2006, no. 4, pp. 32–38.
[5] Lebedev P.F., Tsyplakov Yu.V. Eksperimentalnaya ballistika strategicheskikh LA [Experimental ballistics of strategic aircraft]. In: Strategicheskoe raketnoe vooruzhenie. Kniga 1 [Strategic missile weapons. Book 1]. Moscow, 4 TsNII Publ., 2003, pp. 261–278.
[6] Kazakov G.V., Kotyashev N., Lukin V.L., Mikhaylov S.N. Strategicheskaya stabilnost — Strategic stability, 2019, no. 2, pp. 37–42.
[7] Galaktionov V.S. Dis.…dokt. tekhn. nauk [Dr. Eng. Sc. Diss.]. USSR MoD, 1983, 350 p.
[8] Galaktionov V.S., Kotyashev N.N. Strategicheskaya stabilnost — Strategic stability, 2014, no. 3, pp. 7–13.
[9] Kazakov G.V., Kotyashev N.N., Kunavin V.I. Sposob tseleraspredeleniya dlya ballisticheskikh LA s razdeliayuschimisya golovnymi chastyami (shifr «Libratsiya») [Method of target distribution for ballistic aircraft with separating heads (code “Libration”)]. Patent RF no. 2561703, 2015.
[10] Zakharov V.N., Kotyashev N.N., Mikhailov S.N. Dvoynye tekhnologii — Dual technologies, 2018, no. 3, pp. 40–46.
[11] Petukhov G.B., Yakunin V.I. Metodologicheskie osnovy vneshnego proektirovaniya tselenapravlennykh protsessov i tseleustremlennykh sistem [Methodological foundations of external design of targeted processes and goal-seeking systems]. Moscow, AST Publ., 2006, 504 p.
[12] Garagan S.A., Kotyashev N.N. Oboronnaya tekhnika (Defense technology), 1995, no. 7, pp. 53–56.
[13] Kazakov G.V., Kotyashev N.N., Sprengel A.V. Trudy 4 TsNII MO RF (Coll. Works of CRI 4 of RF MoD), 2008, no. 91, pp. 18–28.
[14] Izyumchenko L.A. Dis. … cand. tekhn. nauk [Cand. Eng. Sc. Diss.]. RF MoD, 1995, 130 p.
[15] Soloviev Yu.S., Kazakov G.V. Voennaya mysl — Military thought, 2016, no. 6, pp. 30–36.
[16] Kazakov G.V., Kotyashev N.N., Klimov S.M. Ob odnom podkhode k otrabotke i otsenke nadezhnosti programmnogo obespecheniya kompleksa sredstv podgotovki dannykh LA [On one approach to testing and evaluating the reliability of the software of the LA data preparation tools complex]. Trudy sektsii 22 XLII Akademicheskikh chteniy po kosmonavtike [Proc. Sect. 22 XLII Acad. Readings in Cosmonautics]. Moscow, 2018, pp. 450–458.
[17] Andreev A.G., Kazakov G.V., Kotyashev N.N. Trudy 4 TsNII MO RF (Coll. Works of CRI 4 of RF MoD), 2018, no. 128, vol. 1, pp. 7–19.
[18] Andreev A.G., Kazakov G.V., Soloviev Yu.S. Izvestiya VA RVSN imeni Petra Velikogo (Bulletin of Military Academia of Srategic Missile Forces n. a. Peter the Great), 2018, no. 280, pp. 26–38.