STAMPS simulates either three- or six-degree-of-freedom cases for all spacecraft flight phases using translated HAL flight software or generic GN&C models. Single or multiple trajectories can be simulated for use in optimization and dispersion analysis. It includes math models for the vehicle and environment, and currently features a "C" version of shuttle onboard flight software. The STAMPS software is used for mission planning and analysis within ascent/descent, rendezvous, proximity operations, and navigation flight design areas
The Shuttle Mission Simulator utilizes four CGI (Computer Generated Image) systems. Orbit simulation...
The Space Station Attitude Control System software test-bed provides a rigorous environment for the ...
Computer program for trajectory optimization and payload maximization in multistage launch vehicle
Within the Consultative Committee for Space Data Systems (CCSDS), there is an effort to standardize ...
Cockpit Avionics Prototyping Environment (CAPE) is a computer program that simulates the functions o...
Over the past five years, the Flight Dynamics Division of the National Aeronautics and Space Adminis...
A computer program has been developed to provide a common interface for all space mission data, and ...
This program was developed to fill a need within the Wallops Flight Facility workflow for automation...
Computer programs provide preliminary trajectory and guidance information required for feasibility s...
A computer program called phxlrsim simulates the behavior of the radar system used as an altimeter a...
A nonlinear, six degree of freedom, digital computer simulation of a vehicle which has constant mass...
This position with the Simulation and Graphics Branch (ER7) at Johnson Space Center (JSC) provided a...
Dynamic programming and multistage decision processes in guidance, flight mechanics, and trajectory ...
For Orion missions beyond low Earth orbit (LEO), the Guidance, Navigation, and Control (GN&C) system...
The High Fidelity Relative Motion Program (HFRMP), a trajectory/attitude numerical integration progr...
The Shuttle Mission Simulator utilizes four CGI (Computer Generated Image) systems. Orbit simulation...
The Space Station Attitude Control System software test-bed provides a rigorous environment for the ...
Computer program for trajectory optimization and payload maximization in multistage launch vehicle
Within the Consultative Committee for Space Data Systems (CCSDS), there is an effort to standardize ...
Cockpit Avionics Prototyping Environment (CAPE) is a computer program that simulates the functions o...
Over the past five years, the Flight Dynamics Division of the National Aeronautics and Space Adminis...
A computer program has been developed to provide a common interface for all space mission data, and ...
This program was developed to fill a need within the Wallops Flight Facility workflow for automation...
Computer programs provide preliminary trajectory and guidance information required for feasibility s...
A computer program called phxlrsim simulates the behavior of the radar system used as an altimeter a...
A nonlinear, six degree of freedom, digital computer simulation of a vehicle which has constant mass...
This position with the Simulation and Graphics Branch (ER7) at Johnson Space Center (JSC) provided a...
Dynamic programming and multistage decision processes in guidance, flight mechanics, and trajectory ...
For Orion missions beyond low Earth orbit (LEO), the Guidance, Navigation, and Control (GN&C) system...
The High Fidelity Relative Motion Program (HFRMP), a trajectory/attitude numerical integration progr...
The Shuttle Mission Simulator utilizes four CGI (Computer Generated Image) systems. Orbit simulation...
The Space Station Attitude Control System software test-bed provides a rigorous environment for the ...
Computer program for trajectory optimization and payload maximization in multistage launch vehicle