Both systems had full attitude command; the more complex system (Type 1) also had translational velocity command. The systems were applied to existing models of a VTOL lift-fan transport and the AV-8A Harrier. Simulated landings were made on a model of a DD963 Spruance-class destroyer. It was concluded that acceptable transitions and vertical landings can be performed, using the Type 1 system, in free-air turbulence up to 2.5 m/sec and sea state 6 and, using the Type 2 system, in free-air turbulence up to 1.5 m/sec and sea state 4
A fixed-base simulator study was conducted to determine the minimum acceptable level of longitudinal...
This paper describes three government-conducted, piloted flight simulations of the Grumman Design 69...
The development of data bases and real time techniques to improve the realism of sea state, bow and ...
Using a generalized simulation model, a moving-base simulation of a lift-fan short takeoff/vertical ...
Using a generalized simulation model, a moving-base simulation of a lift-fan short takeoff/vertical ...
Transition, approach, and vertical landing tests for VTOL transport in terminal are
Results of a substantial body of ground-based simulation experiments indicate that a high degree of ...
The simulation employed all six rigid-body degrees of freedom and incorporated aerodynamic character...
A mathematical model of a high performance airplane capable of vertical attitude takeoff and landing...
Equations incorporated in a VATOL six degree of freedom off-line digital simulation program and data...
A piloted motion simulator evaluation, using the NASA Ames Vertical Motion Simulator, was conducted ...
A flight simulation program was conducted on the flight simulator for advanced aircraft (FSAA). The ...
Simulated flight test of double-Delta supersonic transport for performance characteristics, handling...
The analysis and design of complex multivariable reliable control systems are considered. High perfo...
Simulation experiments to determine the feasibility of landing V/TOL aircraft on ships at sea were s...
A fixed-base simulator study was conducted to determine the minimum acceptable level of longitudinal...
This paper describes three government-conducted, piloted flight simulations of the Grumman Design 69...
The development of data bases and real time techniques to improve the realism of sea state, bow and ...
Using a generalized simulation model, a moving-base simulation of a lift-fan short takeoff/vertical ...
Using a generalized simulation model, a moving-base simulation of a lift-fan short takeoff/vertical ...
Transition, approach, and vertical landing tests for VTOL transport in terminal are
Results of a substantial body of ground-based simulation experiments indicate that a high degree of ...
The simulation employed all six rigid-body degrees of freedom and incorporated aerodynamic character...
A mathematical model of a high performance airplane capable of vertical attitude takeoff and landing...
Equations incorporated in a VATOL six degree of freedom off-line digital simulation program and data...
A piloted motion simulator evaluation, using the NASA Ames Vertical Motion Simulator, was conducted ...
A flight simulation program was conducted on the flight simulator for advanced aircraft (FSAA). The ...
Simulated flight test of double-Delta supersonic transport for performance characteristics, handling...
The analysis and design of complex multivariable reliable control systems are considered. High perfo...
Simulation experiments to determine the feasibility of landing V/TOL aircraft on ships at sea were s...
A fixed-base simulator study was conducted to determine the minimum acceptable level of longitudinal...
This paper describes three government-conducted, piloted flight simulations of the Grumman Design 69...
The development of data bases and real time techniques to improve the realism of sea state, bow and ...