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Guidance and control of a launch vehicle using a stochastic gradient projection method

โœ Scribed by Fernando Madeira; Atair Rios-Neto


Publisher
Elsevier Science
Year
2000
Tongue
English
Weight
227 KB
Volume
36
Category
Article
ISSN
0005-1098

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โœฆ Synopsis


A recently developed nonlinear programming stochastic projection of the gradient-type technique is applied to get and test novel procedures for tri-dimensional guidance and control of a satellite solid-fuel launch vehicle. Near optimal open-loop and lowfrequency closed-loop solutions are obtained by parametrization of the control history and by considering the satisfaction of boundary constraints unless of speci"ed random errors. Numerical simulations and tests show that the closed-loop solution can cope with the typical model uncertainties and environmental perturbations. A non standard situation of having a fourth stage with a free burning time is tested.


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