Model tests for determination of the structural response of the Apollo command module to water impact.
Model tests for determination of structural response of Apollo command module to water impact
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Model tests for determination of structural response of Apollo command module to water impact
Full-size pilot-controlled docking simulation of Apollo command and service module with lunar module using only visual information
Apollo digital command system to provide means of spacecraft communication and control from ground
Wind tunnel tests of Apollo command module static and dynamic stability characteristics
Scanning Celestial Attitude Determination System /SCADS/ for three axis attitude determination at Command and Data Acquisition /CDA/ station
Flight test evaluation of on-off rate command attitude control system of manned lunar landing research vehicle
Probability distribution of time to first loss of lock investigated by second order phase-locked loop - spacecraft telemetry and command
Radar cross section decrease of Apollo command module due to reentry plasma sheath effects
Dynamic stability of Apollo command module with and without drogue parachutes at low subsonic speeds in spin tunnel
Analysis of crew performance in Apollo command module
Crew performance in Apollo command module during 7-day lunar landing simulations
Lunar orbiter command and telemetry data handling system at deep space stations
Model tests for determination of structural response of Apollo Command Module to water impact
Manual thrust vector control development for Apollo Command and Service Module Stabilization and Control System
This paper discusses a proof-of-concept prototype for ground-based automatic generation of validated rover command sequences from high-level science and engineering activities.
This paper discusses a proof-of-concept prototype for ground-based automatic generation of validated rover command sequences from high-level goals using AI-based planning software.
The Command and Telemetry Dictionary is at the heart of space missions. The C&T Dictionary represents all of the information that is exchanged between the various systems both in space and on the ground. Large amounts of ever-changing information has to be disseminated to all for the various systems and sub-systems throughout all phases of the mission. The typical approach of having each sub-system manage it's own information flow, results in a patchwork of methods within a mission. This leads to significant duplication of effort and potential errors. More centralized methods have been developed to manage this data flow. This presentation will compare two tools that have been developed for this purpose, CCDD and SCIMI that were designed to work with the Core Flight System (cFS).