Instructions for using Vertical Attitude Takeoff and Landing Aircraft Simulation (VATLAS), the digital simulation program for application to vertical attitude takeoff and landing (VATOL) aircraft developed for installation on the NASA Ames CDC 7600 computer system are described. The framework for VATLAS is the Off-Line Simulation (OLSIM) routine. The OLSIM routine provides a flexible framework and standardized modules which facilitate the development of off-line aircraft simulations. OLSIM runs under the control of VTOLTH, the main program, which calls the proper modules for executing user specified options. These options include trim, stability derivative calculation, time history generation, and various input-output options
Transition, approach, and vertical landing tests for VTOL transport in terminal are
This paper describes the integration of MATLAB Simulink(Registered TradeMark) models into the Vertic...
A conceptual design study was performed of a vertical attitude takeoff and landing (VATOL) fighter/a...
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...
Both systems had full attitude command; the more complex system (Type 1) also had translational velo...
The V/STOL Aircraft Propulsive Effects (VAPE) computerized prediction method is evaluated. The progr...
A computerized prediction method known as the Vought V/STOL Aircraft Propulsive Effects computer pro...
A standard kinematic model for aircraft simulation exists at NASA-Ames on a variety of computer syst...
A computer program was developed to integrate avionics research in navigation, guidance, controls, a...
Simulator study of flight management task performance during low visibility approach and landing usi...
The VTOL approach and landing test (VALT) adaptive software is documented. Two self-adaptive algorit...
The Ames Research Center Vertical Motion Simulator (VMS) is described in terms useful to the researc...
A short-takeoff and landing (STOL) systems simulation model has been developed and implemented in a ...
The optimal control model (OCM) of the human operator is used to predict the effect of simulator cha...
Transition, approach, and vertical landing tests for VTOL transport in terminal are
This paper describes the integration of MATLAB Simulink(Registered TradeMark) models into the Vertic...
A conceptual design study was performed of a vertical attitude takeoff and landing (VATOL) fighter/a...
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...
Both systems had full attitude command; the more complex system (Type 1) also had translational velo...
The V/STOL Aircraft Propulsive Effects (VAPE) computerized prediction method is evaluated. The progr...
A computerized prediction method known as the Vought V/STOL Aircraft Propulsive Effects computer pro...
A standard kinematic model for aircraft simulation exists at NASA-Ames on a variety of computer syst...
A computer program was developed to integrate avionics research in navigation, guidance, controls, a...
Simulator study of flight management task performance during low visibility approach and landing usi...
The VTOL approach and landing test (VALT) adaptive software is documented. Two self-adaptive algorit...
The Ames Research Center Vertical Motion Simulator (VMS) is described in terms useful to the researc...
A short-takeoff and landing (STOL) systems simulation model has been developed and implemented in a ...
The optimal control model (OCM) of the human operator is used to predict the effect of simulator cha...
Transition, approach, and vertical landing tests for VTOL transport in terminal are
This paper describes the integration of MATLAB Simulink(Registered TradeMark) models into the Vertic...
A conceptual design study was performed of a vertical attitude takeoff and landing (VATOL) fighter/a...