Add to ORKGA study was conducted to identify a broad base of payload control and display requirements for space missions. The subjects discussed are: (1) functional requirements and allocation analysis, (2) control and display generic device matrix, (3) control functional requirements, and (4) display functional requirements. Specific applications of payload control and display requirements for various disciplines are defined
System concepts were characterized in order to define cost versus benefits for autonomous functional...
User technology requirements are identified in relation to needed technology advancement for future ...
Herein, the term mission control will be taken quite broadly to include both ground and space based ...
The results of the Payload Specialist Station study are summarized. An optimum aft flight deck (AFD)...
Technology advances needed for an overall mission model standpoint as well as those for individual s...
The NASA orbiter spacecraft incorporates a complex array of systems, displays and controls. The inco...
Facilities are described on which detailed preliminary design was undertaken and which may be used o...
An analysis of the critical parameters involved in designing systems for spacecraft maneuvers involv...
Concepts for vehicle and payload avionics architectures for future NASA programs, including the Assu...
The controls and displays (C&D) required at the Orbiter aft-flight deck (AFD) and the core C&D requi...
The access schema developed to access both individual switch functions as well as automated or semia...
Optimization study of computation and display requirements for human control of reusable orbital tra...
A study was conducted to derive and collect payload information on the anticipated space processing ...
The space shuttle main engine (SSME) presented new requirements in the design of controls for large ...
The findings of a study to define the required payloads for conducting life science experiments in s...
System concepts were characterized in order to define cost versus benefits for autonomous functional...
User technology requirements are identified in relation to needed technology advancement for future ...
Herein, the term mission control will be taken quite broadly to include both ground and space based ...
The results of the Payload Specialist Station study are summarized. An optimum aft flight deck (AFD)...
Technology advances needed for an overall mission model standpoint as well as those for individual s...
The NASA orbiter spacecraft incorporates a complex array of systems, displays and controls. The inco...
Facilities are described on which detailed preliminary design was undertaken and which may be used o...
An analysis of the critical parameters involved in designing systems for spacecraft maneuvers involv...
Concepts for vehicle and payload avionics architectures for future NASA programs, including the Assu...
The controls and displays (C&D) required at the Orbiter aft-flight deck (AFD) and the core C&D requi...
The access schema developed to access both individual switch functions as well as automated or semia...
Optimization study of computation and display requirements for human control of reusable orbital tra...
A study was conducted to derive and collect payload information on the anticipated space processing ...
The space shuttle main engine (SSME) presented new requirements in the design of controls for large ...
The findings of a study to define the required payloads for conducting life science experiments in s...
System concepts were characterized in order to define cost versus benefits for autonomous functional...
User technology requirements are identified in relation to needed technology advancement for future ...
Herein, the term mission control will be taken quite broadly to include both ground and space based ...