Add to ORKGThe Space Shuttle avionics system, which was conceived in the early 1970's and became operational in the 1980's represents a significant advancement of avionics system technology in the areas of systems and redundacy management, digital data base technology, flight software, flight control integration, digital fly-by-wire technology, crew display interface, and operational concepts. The origins and the evolution of the system are traced; the requirements, the constraints, and other factors which led to the final configuration are outlined; and the functional operation of the system is described. An overall system block diagram is included
A flight computer functional executive design for the reusable shuttle is presented. The design is g...
The engineering design for the Shuttle Missions Simulator is presented in sections, with each sectio...
The tasks involved in the Space Shuttle Development Program are discussed. The ten major characteris...
Conceptual design development of space shuttle integrated avionics system emphasizing necessary elec...
The space shuttle digital, fly by wire, flight control system presents an interesting challenge in a...
The early problems and the solutions developed to provide the required quality software needed to su...
Results of alternate avionics system studies for the space shuttle are presented that reduce the cos...
The background of the shuttle avionics system design and the unique drivers associated with the redu...
Completion of the final Space Shuttle flight marks the end of a significant era in Human Spaceflight...
The space shuttle main engine (SSME) presented new requirements in the design of controls for large ...
The Real Time Data System (RTDS) Project was undertaken in 1987 to introduce new concepts and techno...
Results are presented of systems analyses of the avionics software of the space shuttle orbiter
Conference on ground operations, flight operations, and safety for space shuttle program - Vol.
Space Shuttle chronology; Space Shuttle comparison; Cost comparison; Performance; Program ground rul...
A functional design of software executive system for the space shuttle avionics computer is presente...
A flight computer functional executive design for the reusable shuttle is presented. The design is g...
The engineering design for the Shuttle Missions Simulator is presented in sections, with each sectio...
The tasks involved in the Space Shuttle Development Program are discussed. The ten major characteris...
Conceptual design development of space shuttle integrated avionics system emphasizing necessary elec...
The space shuttle digital, fly by wire, flight control system presents an interesting challenge in a...
The early problems and the solutions developed to provide the required quality software needed to su...
Results of alternate avionics system studies for the space shuttle are presented that reduce the cos...
The background of the shuttle avionics system design and the unique drivers associated with the redu...
Completion of the final Space Shuttle flight marks the end of a significant era in Human Spaceflight...
The space shuttle main engine (SSME) presented new requirements in the design of controls for large ...
The Real Time Data System (RTDS) Project was undertaken in 1987 to introduce new concepts and techno...
Results are presented of systems analyses of the avionics software of the space shuttle orbiter
Conference on ground operations, flight operations, and safety for space shuttle program - Vol.
Space Shuttle chronology; Space Shuttle comparison; Cost comparison; Performance; Program ground rul...
A functional design of software executive system for the space shuttle avionics computer is presente...
A flight computer functional executive design for the reusable shuttle is presented. The design is g...
The engineering design for the Shuttle Missions Simulator is presented in sections, with each sectio...
The tasks involved in the Space Shuttle Development Program are discussed. The ten major characteris...