Add to ORKGThree NASA centers: Marshall Space Flight Center (MSFC), Langley Research Center (LaRC), and Johnson...
The .Advanced Launch System. (ALS) Program is a development effort, to identify and validate new tec...
A regular perturbation analysis is presented. Closed-loop simulations were performed with a first or...
Control and stability aspects prior to spacecraft landing, and propulsive assist to landing spacecra...
Ability of pilot to stabilize flexibile launch vehicle during first stage - Saturn V launch vehicl
Feasibility and reliability analysis in use of pilots to guide and control launch vehicles of Saturn...
Analytical methods for dynamic stability analyses of large launch vehicles during flight through and...
Mathematical model for determining minimax attitude control of aeroballistic launch vehicles - stabi...
Determination of launch vehicle characteristics using dynamic scale models, Vol.
Aspects of an attitude control system were studied and developed for a large space base that is stru...
The baseline stability margins for NASA's Space Launch System (SLS) launch vehicle were generated vi...
Impedance testing for flight control system parameters in studies of launch vehicle dynamic stabilit
Thrust vector deflection angle requirements for controlling solid propellant launch vehicl
Digital polynomial and adaptive feedback control system techniques for large launch vehicle guidance...
The space shuttle digital, fly by wire, flight control system presents an interesting challenge in a...
Three NASA centers: Marshall Space Flight Center (MSFC), Langley Research Center (LaRC), and Johnson...
The .Advanced Launch System. (ALS) Program is a development effort, to identify and validate new tec...
A regular perturbation analysis is presented. Closed-loop simulations were performed with a first or...
Control and stability aspects prior to spacecraft landing, and propulsive assist to landing spacecra...
Ability of pilot to stabilize flexibile launch vehicle during first stage - Saturn V launch vehicl
Feasibility and reliability analysis in use of pilots to guide and control launch vehicles of Saturn...
Analytical methods for dynamic stability analyses of large launch vehicles during flight through and...
Mathematical model for determining minimax attitude control of aeroballistic launch vehicles - stabi...
Determination of launch vehicle characteristics using dynamic scale models, Vol.
Aspects of an attitude control system were studied and developed for a large space base that is stru...
The baseline stability margins for NASA's Space Launch System (SLS) launch vehicle were generated vi...
Impedance testing for flight control system parameters in studies of launch vehicle dynamic stabilit
Thrust vector deflection angle requirements for controlling solid propellant launch vehicl
Digital polynomial and adaptive feedback control system techniques for large launch vehicle guidance...
The space shuttle digital, fly by wire, flight control system presents an interesting challenge in a...
Three NASA centers: Marshall Space Flight Center (MSFC), Langley Research Center (LaRC), and Johnson...
The .Advanced Launch System. (ALS) Program is a development effort, to identify and validate new tec...
A regular perturbation analysis is presented. Closed-loop simulations were performed with a first or...