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A nonlinear programming approach to space shuttle trajectory optimization (1974)

Brusch, R. G.

Springer

Journal of optimization theory and applications 13 (1974), S. 94-118

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ISSN: 1573-2878

Keywords: Nonlinear programming ; penalty-function methods ; trajectories ; state variable constraints ; flight mechanics

Source: Springer Online Journal Archives 1860-2000

Topics: Mathematics

Notes: Abstract Space shuttle trajectory design requires the optimization of highly-constrained, branched, atmospheric trajectories. This paper presents a general mathematical model for trajectory optimization incorporating multiple simulation sections, state variable discontinuities, subarc elimination, branching, and six types of equality and inequality constraints. A solution is sought using a nonlinear programming approach based on SUMT, the sequential unconstrained minimization technique. Results of the numerical solution of a highly constrained space shuttle reentry problem are presented.

Type of Medium: Electronic Resource

URL: http://dx.doi.org/10.1007/BF00935611

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