Add to ORKGAbility of pilot to stabilize flexibile launch vehicle during first stage - Saturn V launch vehicl
Examples of control problems occurring during flight tests of fighter aircraft are well documented. ...
Fixed-base visual simulation study for ability determination of onboard pilot during landin
From the control point of view, spacecraft are classified into two main groups: those for which the ...
Piloted simulation of manual guidance techniques for upper stages of Saturn V launch vehicl
Feasibility and reliability analysis in use of pilots to guide and control launch vehicles of Saturn...
Evaluation of pilot describing function method applied to manual control analysis of large flexible ...
The effectiveness of attitude control laws that are designed to reduce bending moment loads and impr...
Launch vehicle flight control system and relation to stability requirements and dynamic response
The flight control system for the NASA Space Launch System (SLS) employs a control architecture that...
Three NASA centers: Marshall Space Flight Center (MSFC), Langley Research Center (LaRC), and Johnson...
A robust and flexible autopilot architecture for NASA's Space Launch System (SLS) family of launch v...
Control requirements of Controlled Configured Design Approach vehicles with far-aft center of gravit...
In this paper we present a technique for approximating the short-period dynamics of an exploration-c...
Piloted simulation studies of Saturn 5 launch vehicle manual backup guidance and contro
Computational and display requirements for man-computer guidance and control techniques for reusable...
Examples of control problems occurring during flight tests of fighter aircraft are well documented. ...
Fixed-base visual simulation study for ability determination of onboard pilot during landin
From the control point of view, spacecraft are classified into two main groups: those for which the ...
Piloted simulation of manual guidance techniques for upper stages of Saturn V launch vehicl
Feasibility and reliability analysis in use of pilots to guide and control launch vehicles of Saturn...
Evaluation of pilot describing function method applied to manual control analysis of large flexible ...
The effectiveness of attitude control laws that are designed to reduce bending moment loads and impr...
Launch vehicle flight control system and relation to stability requirements and dynamic response
The flight control system for the NASA Space Launch System (SLS) employs a control architecture that...
Three NASA centers: Marshall Space Flight Center (MSFC), Langley Research Center (LaRC), and Johnson...
A robust and flexible autopilot architecture for NASA's Space Launch System (SLS) family of launch v...
Control requirements of Controlled Configured Design Approach vehicles with far-aft center of gravit...
In this paper we present a technique for approximating the short-period dynamics of an exploration-c...
Piloted simulation studies of Saturn 5 launch vehicle manual backup guidance and contro
Computational and display requirements for man-computer guidance and control techniques for reusable...
Examples of control problems occurring during flight tests of fighter aircraft are well documented. ...
Fixed-base visual simulation study for ability determination of onboard pilot during landin
From the control point of view, spacecraft are classified into two main groups: those for which the ...