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Dynamic System Control Dispatch: A Global Optimization Approach

In: Modeling and Optimization in Space Engineering

Author

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  • Giorgio Fasano

    (Thales Alenia Space)

Abstract

This work originates from research related to an optimal control dispatch problem in space: the problem in question is presented in detail in another chapter of this volume by Anselmi et al. (Control propellant minimization for the next generation gravity mission. In: Fasano G, Pintér JD (eds) Modeling and optimization in space engineering – state of the art and new challenges. Springer, New York, 2019). Here we discuss the general issue of dispatching the control of a dynamic system through a number of actuators, presenting a novel model development and algorithmic solution approach. A control law, expressed in terms of total force and torque demand, represents the operational scenario. This gives rise to a very challenging optimization problem, concerning the actuator accommodation and utilization. Following the model formulation, a dedicated heuristic approach–involving nonlinear and mixed integer linear programming–is proposed. The numerical results presented illustrate the efficiency of the methodology adopted.

Suggested Citation

  • Giorgio Fasano, 2019. "Dynamic System Control Dispatch: A Global Optimization Approach," Springer Optimization and Its Applications, in: Giorgio Fasano & János D. Pintér (ed.), Modeling and Optimization in Space Engineering, pages 87-110, Springer.
    • Handle: RePEc:spr:spochp:978-3-030-10501-3_4
    DOI: 10.1007/978-3-030-10501-3_4
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    Keywords

    90C06; 90C11; 90C26; 90C30; 90C59; 90C90;
    All these keywords.

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