Abstract
Consideration was given to the problem of suboptimal control of the flight vehicle in atmosphere which was solved numerically. The results presented corroborate the efficiency of this procedure. The present paper is distinguished for the fact that the complex nonlinear boundary problem was solved using a finite number of arithmetic operations.
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Ivanov, A.P. and Ostov, Yu.Ya., Duality and Principle of Extension in the Problem of Flight Dynamics, in Metody matematicheskogo modelirovaniya i informatsionnye tekhnologii, Tr. Ins. Prikl. Mat. Issled., Karel. Nauchn. Tsentr. Ross. Akad. Nauk (Methods of Mathematical Modeling and Information Technologies, Proc. Inst. of Applied Mathematical Research, Karelian Research Centre of Russ. Acad. Sci.), Petrozavodsk: Inst. Prikl. Mat. Issl., 2006, vol. 7, pp. 26–34.
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Original Russian Text © Yu.Ya. Ostov, A.P. Ivanov, 2014, published in Avtomatika i Telemekhanika, 2014, No. 2, pp. 146–155.
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Ostov, Y.Y., Ivanov, A.P. Method of optimization in flight dynamics. Autom Remote Control 75, 294–301 (2014). https://doi.org/10.1134/S000511791402009X
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DOI: https://doi.org/10.1134/S000511791402009X