Add to ORKGFeasibility and reliability analysis in use of pilots to guide and control launch vehicles of Saturn 5 clas
Design of air bearing supported test platforms for dynamic simulation of space vehicle attitude cont...
Analysis and design of space vehicle control systems - short period dynamics of attitude control dur...
Launch vehicle flight control system and relation to stability requirements and dynamic response
Evaluation of pilot describing function method applied to manual control analysis of large flexible ...
Ability of pilot to stabilize flexibile launch vehicle during first stage - Saturn V launch vehicl
Piloted simulation of manual guidance techniques for upper stages of Saturn V launch vehicl
Digital six-degrees-of-freedom, open loop Saturn 5 first stage flight evaluation simulation program ...
The optimal control model for pilot vehicle systems was used to develop a methodology for predicting...
Piloted simulation studies of Saturn 5 launch vehicle manual backup guidance and contro
Computer simulation feasibility study for Saturn launch vehicle and support equipmen
Self adaptive control techniques for attitude control on Saturn 5 launch vehicle
A pilot model analysis was performed that relates pilot control compensation, pilot aircraft system...
Computerized and dynamic simulation models for spacecraft systems - mathematical models for predicti...
An analysis of the critical parameters involved in designing systems for spacecraft maneuvers involv...
A piloted simulator was used to evaluate the flight path angle control capabilities of a system that...
Design of air bearing supported test platforms for dynamic simulation of space vehicle attitude cont...
Analysis and design of space vehicle control systems - short period dynamics of attitude control dur...
Launch vehicle flight control system and relation to stability requirements and dynamic response
Evaluation of pilot describing function method applied to manual control analysis of large flexible ...
Ability of pilot to stabilize flexibile launch vehicle during first stage - Saturn V launch vehicl
Piloted simulation of manual guidance techniques for upper stages of Saturn V launch vehicl
Digital six-degrees-of-freedom, open loop Saturn 5 first stage flight evaluation simulation program ...
The optimal control model for pilot vehicle systems was used to develop a methodology for predicting...
Piloted simulation studies of Saturn 5 launch vehicle manual backup guidance and contro
Computer simulation feasibility study for Saturn launch vehicle and support equipmen
Self adaptive control techniques for attitude control on Saturn 5 launch vehicle
A pilot model analysis was performed that relates pilot control compensation, pilot aircraft system...
Computerized and dynamic simulation models for spacecraft systems - mathematical models for predicti...
An analysis of the critical parameters involved in designing systems for spacecraft maneuvers involv...
A piloted simulator was used to evaluate the flight path angle control capabilities of a system that...
Design of air bearing supported test platforms for dynamic simulation of space vehicle attitude cont...
Analysis and design of space vehicle control systems - short period dynamics of attitude control dur...
Launch vehicle flight control system and relation to stability requirements and dynamic response