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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Published in | Automatica (Oxford) Vol. 8; no. 2; pp. 153 - 161 |
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Main Authors | , |
Format | Journal Article |
Language | English |
Published |
Elsevier Ltd
01.01.1972
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Online Access | Get full text |
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