Numerical comparison is made in idealized problem wherein computations are simple enough not to require machine computation; orthodox solution involving usual Lagrange multiplier associated with kinematical restraint, and unorthodox solution in which this multiplier is treated as identically zero; pertinence to problem of rocket trajectory.
Approximations in flight optimization problems
Aerospace Eng
Aerospace Engineering ; 20 , n 9
1961
Article (Journal)
English
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Unified Aeroelastic and Flight Dynamic Formulation via Rational Function Approximations
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