Preliminary entry guidance and autopilot software formulations, for use in the Mission Control Center (MCC) entry processor, are presented. The MCC requirements are met by a definition of coordinate systems, a list of parameter definitions for the software formulations, a description of the entry guidance detailed formulation requirements, a description of the detailed autopilot formualtion requirements, a description of the targeting routine, and a set of formulation flow charts
The software utilized for image correction accuracy measurement is described. The correlation analys...
General criteria for design of equipment and facilities to be used at Kennedy Space Cente
A nitrogen supply subsystem based on the dissociation of hydrazine into a mixture of hydrogen and ni...
The level C requirements for the shuttle orbiter terminal area energy management (TAEM) guidance and...
An 0.8 percent fuel savings was achieved by a reduction in engine bleed air through the use of cabin...
The baseline products, schedules, and resource requirements for the Mission Planning and Analysis Di...
Mathematical models and orbital mechanics for space shuttle guidance, control, and navigation during...
The computer code for the trajectory processor (#TRAJ) of the high fidelity relative motion program ...
A three-person capacity preprototype vapor compression distillation subsystem for recovering potable...
The Mars Rover Laser Scanning system uses a precision laser pointing mechanism, a photodetector arra...
The level C software formulations requirements for the entry guidance and the simplified autopilot t...
The functional requirements and the configuration of the data base management system are described. ...
The results of an effort to plan a final verification wind tunnel test to validate the recommended c...
A definition of the level C requirements for onboard maneuver targeting software is provided. Includ...
A research and development program was successfully completed towards the development of a method of...
The software utilized for image correction accuracy measurement is described. The correlation analys...
General criteria for design of equipment and facilities to be used at Kennedy Space Cente
A nitrogen supply subsystem based on the dissociation of hydrazine into a mixture of hydrogen and ni...
The level C requirements for the shuttle orbiter terminal area energy management (TAEM) guidance and...
An 0.8 percent fuel savings was achieved by a reduction in engine bleed air through the use of cabin...
The baseline products, schedules, and resource requirements for the Mission Planning and Analysis Di...
Mathematical models and orbital mechanics for space shuttle guidance, control, and navigation during...
The computer code for the trajectory processor (#TRAJ) of the high fidelity relative motion program ...
A three-person capacity preprototype vapor compression distillation subsystem for recovering potable...
The Mars Rover Laser Scanning system uses a precision laser pointing mechanism, a photodetector arra...
The level C software formulations requirements for the entry guidance and the simplified autopilot t...
The functional requirements and the configuration of the data base management system are described. ...
The results of an effort to plan a final verification wind tunnel test to validate the recommended c...
A definition of the level C requirements for onboard maneuver targeting software is provided. Includ...
A research and development program was successfully completed towards the development of a method of...
The software utilized for image correction accuracy measurement is described. The correlation analys...
General criteria for design of equipment and facilities to be used at Kennedy Space Cente
A nitrogen supply subsystem based on the dissociation of hydrazine into a mixture of hydrogen and ni...