Research on advanced kick stage guidance computer study
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Results for “GUIDANCE”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Arc guidance development work for tack-welded joints
DOWNSTREAM HEAT TRANSFER OF UPSTREAM MASS INJECTION IN SUPERSONIC LAMINAR BOUNDARY LAYER FLOW
Chadbourne, J.↗
R and D reporting - Guidance for technical monitors of NASA contracts
Options and information resources open to NASA monitors
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Application of VLF Navigation and Automatic Calibration of Barometric Altitude Sensing to General Aviation and a National Universal Coordinate System for the Guidance and Control of Air Traffic Final Report
Very low frequency air navigation, automatic calibration of barometric sensing, and universal coordinate system for air traffic control
Litchford, G. B.↗
An Analytical Investigation of Acquisition Techniques and System Integration Studies for a Radar Aircraft Guidance Research Facility
Boresight camera records for angular tracking accuracy of aircraft
Britt, C. L.↗
Some applications of Kalman filtering in space guidance
Linear optimal recursive filtering techniques for space navigation
Bellantoni, J. F.↗
Radio/Optical/Strapdown Inertial Guidance Study for Advanced Kick Stage Applications - Launch Vehicle Data /Tasks 5 and 6/
Data and data plots for launch vehicle configurations used in advanced kick stage applications
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NASA space vehicle design criteria, guidance and control - Entry vehicle control
Stabilization and control systems for reentry vehicle
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Investigations of the potential performance characteristics of selected contact lubricants for applications in miniature slip-ring capsules of the type used in ST 124 M stabilized inertial guidance platforms Final technical report, 27 Mar. 1968 - 30 Apr. 1970
Performance characteristics of liquid and solid lubricants for contacts of miniature slip-ring capsules
Baker, J. B.↗
Performance of Apollo block 2 thrust vector control using the PGNCS /Primary Guidance Navigation and Control System/ - Project Apollo
Computerized performance evaluation of Apollo thrust vector digital autopilot control system
Smith, E. E., Jr.↗
Space shuttle trajectory management, navigation, guidance, and control during approach and landing Interim report
Trajectory control and optimization for space shuttle approach and landing
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The use of statistics in guidance analysis
Statistical analysis of space navigation systems based on multivariate Gaussian distributions and linear perturbation theory
Galli, D. H.↗
Preliminary analysis for lunar roving vehicle study, ground data systems and operations. Volume 1 - Roving vehicle guidance /Remote driving study/
Remote driving of lunar roving vehicle by superimposing driving aids on TV panorama
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Orbiting Geophysical Observatory Attitude Control Subsystem Design Survey. NASA/ERC Design Criteria Program, Guidance and Control
This design survey summarizes the history of the Orbiting Geophysical Observatories' (OGO) Attitude Control Subsystem (ACS) from the proposal phase through current flight experience. Problems encountered in design, fabrication, test, and on orbit are discussed. It is hoped that the experiences of the OGO program related here will aid future designers.
Mc Kenna, K. J.↗
A parameter dependent spacecraft guidance boundary value problem
Spacecraft trajectory initial conditions expressions as parameters dependent functions, applying results to Mars lander mission
Cefola, P. J.↗
The STAR computer - A self-testing-and- repairing computer for spacecraft guidance, control, and automatic maintenance
Successful planetary exploration missions have been completed by unmanned Mariner spacecraft, which were designed at the Jet Propulsion Laboratory. Mariner II completed a 109-day flyby mission to Venus on December 14, 1962. This mission was followed by the flyby of Mars and return of 21 historic photographs of its surface by Mariner IV in July 1965. Further successful missions followed: Mariner V to Venus in 1967, Mariners VI and VII to Mars in 1969. In all of these missions, a Central Computer and Sequencer onboard the spacecraft was used to provide on-board control functions, although complete ground backup was also available.
Algirdas Avizienist↗
Mascot - A new concept in guidance
Trajectory algorithm for complete trajectory from liftoff to landing with optimal control and onboard flight computer for use in manned space shuttle
Baker, C. D.↗
A microwave beam power transfer and guidance system for use in an orbital astronomy support facility Final report, 10 Dec. 1969 - 10 Dec. 1970
Employment of microwave beams for transferring power between satellites
Brown, W. C.↗