Through Optimization of Aerospace Vehicle Trajectories by the Pontryagin Maximum Principle
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Through Optimization of Aerospace Vehicle Trajectories by the Pontryagin Maximum Principle
Filatyev, Alexander S.; Petukhov, Vyacheslav G.
Springer International Publishing AG
03/2025
265
Dura
9783031807558
Pré-lançamento - envio 15 a 20 dias após a sua edição
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The Pontryagin Maximum Principle For Trajectory Optimization.- Optimization Of Aerospace Vehicle Trajectories In The Atmosphere Based On The Pontryagin Maximum Principle.- Qualitative Analysis Of The Aerodynamic Forces Effect On The Optimal Ascent Trajectories And Control.- The Through Optimization Of Branching Trajectories With A Finite Set Of Branches.- The Through Optimization Of Branching Trajectories With A Continuum Of Branches.- Investigation Of Optimal Branching Trajectories Of Various Types Of Space Transportation Systems.- Mathematical Models Of A Spacecraft With An Electric Propulsion For Trajectory Optimization Problems.- Optimization Of Limited-Power Interplanetary Trajectories.- Optimization Of Interplanetary Trajectories For A Limited-Thrust Spacecraft.- Optimization Of Complex Schemes Of Interplanetary Low Thrust Transfers.
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Space Transportation Systems;Spacecraft;Electric Propulsion;Pontryagin maximum principle;Space Physics
The Pontryagin Maximum Principle For Trajectory Optimization.- Optimization Of Aerospace Vehicle Trajectories In The Atmosphere Based On The Pontryagin Maximum Principle.- Qualitative Analysis Of The Aerodynamic Forces Effect On The Optimal Ascent Trajectories And Control.- The Through Optimization Of Branching Trajectories With A Finite Set Of Branches.- The Through Optimization Of Branching Trajectories With A Continuum Of Branches.- Investigation Of Optimal Branching Trajectories Of Various Types Of Space Transportation Systems.- Mathematical Models Of A Spacecraft With An Electric Propulsion For Trajectory Optimization Problems.- Optimization Of Limited-Power Interplanetary Trajectories.- Optimization Of Interplanetary Trajectories For A Limited-Thrust Spacecraft.- Optimization Of Complex Schemes Of Interplanetary Low Thrust Transfers.
Este título pertence ao(s) assunto(s) indicados(s). Para ver outros títulos clique no assunto desejado.
