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Features of problems in the optimization of the characteristics of aircraft and spacecraft with respect to cost effectiveness

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Cybernetics Aims and scope

Conclusions

  1. 1.

    The above procedure makes it possible to simplity the optimization of the control and parameters of aircraft and spacecraft.

    Indeed, the optimization process can be divided into three stages, each of which can be optimized independently of the others. The results of optimization of the separate stages are combined according to the weight of the orbital apparatus (GOA=G1).

    A similar simplification results from the division of the cost of the planned operation as in (4), and from the transformations in (6) and (8) of this cost and its components.

  2. 2)

    The characteristic division of the optimality criterion into its component parts in the above procedure makes it possible to reveal the design parameters occurring in the arguments of the function relation which formalizes mathematically the cost of the planned operation.

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Literature Cited

  1. P. M. Morse and G. E. Kimball, Methods of Operations Research [Russian translation], izd-vo Sovetskoe Radio, Moscow, 1956.

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  2. G. Kh. Gud and R. E. Makol, Systematic Techniques Introduction to the Design of Large Systems [in Russian], Izd-vo Sovetskoe Radio, Moscow, 1962.

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  3. R. Bellman, Dynamic Programming [Russian translation], IL, Moscow, 1960.

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  4. E. S. Venttsel, Introduction to Operations Research [in Russian], Izd-vo Sovetskoe Radio, Moscow, 1964.

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  5. V. S. Mikhalevich, Yu. M. Ermol'ev, V. V. Shkura, and N. Z. Shor, “Complex systems and the solution of extremal problems,” Kibernetika, no. 5, Kiev, 1967.

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Authors
  1. A. I. Egorov
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Additional information

Translated from Kibernetika, Vol. 5, No. 2, pp 84–89, March–April, 1969.

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Egorov, A.I. Features of problems in the optimization of the characteristics of aircraft and spacecraft with respect to cost effectiveness. Cybern Syst Anal 5, 221–226 (1969). https://doi.org/10.1007/BF01071092

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  • DOI: https://doi.org/10.1007/BF01071092

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