Minimum time thrust start-up of a nuclear rocket with integro-differential constraints

The minimum time thrust start-up of a nuclear rocket gives rise to an optimal control problem where the state representing the exhaust propellant must satisfy an integro-differential equation and an inequality constraint. It is shown that by defining an appropriate Hamiltonian function, Pontryagin&#...

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Bibliographic Details
Published inAutomatica (Oxford) Vol. 8; no. 2; pp. 153 - 161
Main Authors Pym, J.W., Shen, C.N.
Format Journal Article
LanguageEnglish
Published Elsevier Ltd 01.01.1972
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