The computer code for the trajectory processor (#TRAJ) of the high fidelity relative motion program is described. The #TRAJ processor is a 12-degrees-of-freedom trajectory integrator (6 degrees of freedom for each of two vehicles) which can be used to generate digital and graphical data describing the relative motion of the Space Shuttle Orbiter and a free-flying cylindrical payload. A listing of the code, coding standards and conventions, detailed flow charts, and discussions of the computational logic are included
A FORTRAN coded computer program which determines secular variations in mean orbital elements of ear...
The use of the SUDAN computer program for analyzing structural systems for their natural modes and f...
Simple analytical models are presented of the radiometric and statistical processes that are involve...
A research and development program was successfully completed towards the development of a method of...
A three-person capacity preprototype vapor compression distillation subsystem for recovering potable...
The performance of Bosch hardware at the subsystem level (up to five-person capacity) in terms of fi...
The level C requirements for the shuttle orbiter terminal area energy management (TAEM) guidance and...
Utilization in the development of multi-kW low orbit power systems is discussed. The following techn...
A data link system used on a prototype autonomous roving vehicle is described. This system provides ...
The functional requirements and the configuration of the data base management system are described. ...
An algorithm for using electric currents to control pendular oscillations induced by various perturb...
The software utilized for image correction accuracy measurement is described. The correlation analys...
The results of an effort to plan a final verification wind tunnel test to validate the recommended c...
The FORTRAN computer program RAWINPROC accepts output from NASA Wallops computer program METPASS1; a...
The AEROX aerodynamic computer program which provides accurate predictions of induced drag and trim ...
A FORTRAN coded computer program which determines secular variations in mean orbital elements of ear...
The use of the SUDAN computer program for analyzing structural systems for their natural modes and f...
Simple analytical models are presented of the radiometric and statistical processes that are involve...
A research and development program was successfully completed towards the development of a method of...
A three-person capacity preprototype vapor compression distillation subsystem for recovering potable...
The performance of Bosch hardware at the subsystem level (up to five-person capacity) in terms of fi...
The level C requirements for the shuttle orbiter terminal area energy management (TAEM) guidance and...
Utilization in the development of multi-kW low orbit power systems is discussed. The following techn...
A data link system used on a prototype autonomous roving vehicle is described. This system provides ...
The functional requirements and the configuration of the data base management system are described. ...
An algorithm for using electric currents to control pendular oscillations induced by various perturb...
The software utilized for image correction accuracy measurement is described. The correlation analys...
The results of an effort to plan a final verification wind tunnel test to validate the recommended c...
The FORTRAN computer program RAWINPROC accepts output from NASA Wallops computer program METPASS1; a...
The AEROX aerodynamic computer program which provides accurate predictions of induced drag and trim ...
A FORTRAN coded computer program which determines secular variations in mean orbital elements of ear...
The use of the SUDAN computer program for analyzing structural systems for their natural modes and f...
Simple analytical models are presented of the radiometric and statistical processes that are involve...