Flight operations of an unmanned planetary mission.
Ground system design, data processing, digital command and digital-human interface in flight operations problems for unmanned spacecraft on planetary exploration mission
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Ground system design, data processing, digital command and digital-human interface in flight operations problems for unmanned spacecraft on planetary exploration mission
GEOS optical memory and control unit for controlling operation of optical beacon - digital delayed command system with high accuracy real time clock
Design of command and data handling system for orbiting astronomical observatory, and scientific experiments for OAO spacecraft
Microelectronic analog data and digital command control system for transonic dynamic wind tunnel tests of research aircraft models
Spacecraft attitude control and stabilization emphasizing control computers, switching logic, mission requirements and system design
Operational application of the command generator (CG) was examined in detail in a simulation of a flight control system with the augmentor wing jet STOL research aircraft. The basic repertoire of single axis maneuvers and operational constraints are discussed, and the system behavior is tested on a rigorous STOL approach path and as affected by various approximations in the CG synthesis and types of disturbances found in the operational environment. The simulation results indicate that a satisfactory nonlinear system with general maneuvering capabilities throughout the flight envelope was developed which satisfies the basic design objectives while maintaining a practicable degree of simplicity.
Spacecraft and ground equipment of Lunar Orbiter telecommunications system
Brief description of a computer ground checkout and launch control system
Console Computer Interface Adapter (CCIA) to provide communication between flight control consoles and telemetry and command computers of Apollo network
Scanning Celestial Attitude Determination System /SCADS/ for three axis attitude determination at Command and Data Acquisition /CDA/ station
Digital controller using multirate sampling for gain control
Digital Command Network for error-free radio command control of manned and unmanned spacecraft
A discription of the logic design for the digital control equipment is followed by further descriptions of items of particular interest. The means of applying off-sets to the demanded aerial position for over-coming possible inaccuracy of the predicted orbit; and to demand accuratly determined velocities manually; means of conversion from pure binary form to provide displays in terms of angles, and the derivation of analogue voltages for the for the servo-amplifiers are discussed in detail. A critical analysis of the equipment in the light of operational experience concludes the paper.
A systems and operational summary of the Titan 3E/Centaur D-1T program is presented which describes vehicle assembly facilities, launch facilities, and management responsibilities, and also provides detailed information on the following separate systems: (1) mechanical systems, including structural components, insulation, propulsion units, reaction control, thrust vector control, hydraulic systems, and pneumatic equipment; (2) astrionics systems, such as instrumentation and telemetry, navigation and guidance, C-Band tracking system, and range safety command system; (3) digital computer unit software; (4) flight control systems; (5) electrical/electronic systems; and (6) ground support equipment, including checkout equipment.
Digital system gives pilot partial command when primary system fails. Emergency system provides digital control of rigid circulation-control rotor for experimental X-wing aircraft. In addition to centering collective-pitch control, new command provides limited roll control via collective pitch and gyroscopic decoupling in pitch and aerodynamic decoupling.
Operational systems engineering for orbiting satellite, emphasizing digital computer at command and telemetry data acquisition station
A Digital Beam Former Test System was developed to determine the effects of noise, interferers and distortions, and digital implementations of beam forming as applied to the Tracking and Data Relay Satellite 2 (TDRS 2) architectures. The investigation of digital beam forming with application to TDRS 2 architectures, as described in TDRS 2 advanced concept design studies, was conducted by the NASA/Lewis Research Center for NASA/Goddard Space Flight Center. A Test and Control Computer (TCC) was used as the main controlling element of the digital Beam Former Test System. The Test and Control Computer User's Guide for a Digital Beam Former Test System provides an organized description of the Digital Beam Former Test System commands. It is written for users who wish to conduct tests of the Digital Beam forming Test processor using the TCC. The document describes the function, use, and syntax of the TCC commands available to the user while summarizing and demonstrating the use of the commands wtihin DOS batch files.
Command encoder for command data system produces sinusoidal signals by purely digital means.