Add to ORKGThe general functional design and implementation of processors for a space flight design system are briefly described. Discussions of a basetime initialization processor; conic, analytical, and precision coasting flight processors; and an orbit lifetime processor are included. The functions of several utility routines are also discussed
Executive routine primitives and process control for spaceborne computer functional design specifica...
In order to meet the stringent time-critical requirements for real-time man-in-the-loop flight simul...
Functional requirements and preliminary design data were identified for use in the design of all sys...
The general need and requirements for the onboard embedded processors necessary to control and manip...
Component reliability and machine language features of onboard spacecraft digital compute
This final report summarizes the work on the design of a fault tolerant digital computer for aircraf...
A flight computer functional executive design for the reusable shuttle is presented. The design is g...
A study was conducted to determine how major improvements in spacecraft computer systems can be obta...
Data analysis is a process of inspecting, cleaning, transforming, and modeling data to highlight use...
Flight planning requirements were analyzed and a computer system architecture was defined. An evalua...
Advancements in hardware and software technology are summarized with specific emphasis on spacecraft...
The requirements for fault-tolerant computers for flight control of commercial aircraft are examined...
In 1975, the National Aeronautics and Space Administration (NASA) began studies to assess the techni...
In order to meet the stringent time-critical requirements for real-time man-in-the-loop flight simul...
The desirability and feasibility of computer-augmented support for the pre-implementation activities...
Executive routine primitives and process control for spaceborne computer functional design specifica...
In order to meet the stringent time-critical requirements for real-time man-in-the-loop flight simul...
Functional requirements and preliminary design data were identified for use in the design of all sys...
The general need and requirements for the onboard embedded processors necessary to control and manip...
Component reliability and machine language features of onboard spacecraft digital compute
This final report summarizes the work on the design of a fault tolerant digital computer for aircraf...
A flight computer functional executive design for the reusable shuttle is presented. The design is g...
A study was conducted to determine how major improvements in spacecraft computer systems can be obta...
Data analysis is a process of inspecting, cleaning, transforming, and modeling data to highlight use...
Flight planning requirements were analyzed and a computer system architecture was defined. An evalua...
Advancements in hardware and software technology are summarized with specific emphasis on spacecraft...
The requirements for fault-tolerant computers for flight control of commercial aircraft are examined...
In 1975, the National Aeronautics and Space Administration (NASA) began studies to assess the techni...
In order to meet the stringent time-critical requirements for real-time man-in-the-loop flight simul...
The desirability and feasibility of computer-augmented support for the pre-implementation activities...
Executive routine primitives and process control for spaceborne computer functional design specifica...
In order to meet the stringent time-critical requirements for real-time man-in-the-loop flight simul...
Functional requirements and preliminary design data were identified for use in the design of all sys...