Abstract
The paper considers the control design problem of a weather rocket, the latter reaching a maximum height at optimal rocket thrust. A control is sought as a nonlinear dependence of thrust on the height and rate of ascent. Such a control is robust with respect to variations of the air drag model. The genetic programming method is applied to obtain the control.
Similar content being viewed by others
References
Lee, E.B. and Markus, L., Foundations of Optimal Control Theory, New York: Wiley, 1967; Moscow: Nauka, 1972.
Fedorenko, R.P., Priblizhennoe reshenie zadach optimal’nogo upravleniya (Approximate Solution of Optimal Control Problems), Moscow: Nauka, 1978.
Koza, J.R., Genetic Programming: On the Programming of Computers by Means of Natural Selection, Cambridge: MIT Press, 1992.
Holland, J.H., Adaptation in Natural and Artificial Systems, Ann Arbor: University of Michigan, 1975.
Anderson, J.A., Discrete Mathematics with Combinatorics, New Jersey: Prentice Hall, 2002; Moscow: Williams, 2003.
Diveev, A.I. and Sofronova, E.A., Method of Genetic Programming for Automatic Selection of Formulas in the Problem of Structure Synthesis of a Control System, Dynamics of Heterogeneous Systems, Moscow: ISA RAN, KomKniga, 2006. Issue 10(1). pp. 14–26.
Diveev, A.I. and Sofronova, E.A., Problem of Structure Analysis of an Automated Control System, Vest. Ross. Univ. Druzhby Narodov., Ser.: Inzh. Issl., 2007, no. 1, pp. 48–58.
Author information
Authors and Affiliations
Additional information
Original Russian Text © A.I. Diveev, N.A. Severtsev, E.A. Sofronova, 2008, published in Problemy Mashinostroeniya i Nadezhnosti Mashin, 2008, No. 5, pp. 104–108.
About this article
Cite this article
Diveev, A.I., Severtsev, N.A. & Sofronova, E.A. Control design of a weather rocket by genetic programming method. J. Mach. Manuf. Reliab. 37, 501–505 (2008). https://doi.org/10.3103/S1052618808050154
Received:
Published:
Issue Date:
DOI: https://doi.org/10.3103/S1052618808050154