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Three-dimensional g-constrained shuttle boost trajectory optimization using a min-H/secant hybrid algorithm
Three-dimensional g-constrained shuttle boost trajectory optimization using a min-H/secant hybrid algorithm
1975
R. G. Gottlieb
W. T. Fowler
Keywords:
Method of steepest descent
Trajectory optimization
Mach number
Control theory
Calculus of variations
Angle of attack
Space Shuttle
Aerodynamic force
Hybrid algorithm
Mathematics
Correction
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