Optimal External Configuration Design of Unguided Missiles

A simple optimal external configuration design method is proposed that can be used in conceptual and preliminary design stages of an unguided missile development project. Cost and constraint functions are derived from the results of linear time-invariant aeroballistic theory (constant roll rate and...

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Veröffentlicht in:	Journal of spacecraft and rockets 1998-05, Vol.35 (3), p.312-316
Hauptverfasser:	Tanrikulu, Omer, Ercan, Veysi
Format:	Artikel
Sprache:	eng
Schlagworte:	Algorithmic languages Configuration management Constraint theory Curve fitting Functions Missile design Missiles Optimization Subsonic aerodynamics
Online-Zugang:	Volltext
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