Guidance methods for low-thrust space vehicles Cumulative progress report, 1 Jan. 1969 - 31 Jan. 1970
Guidance and control schemes for optimal low-thrust Earth-Mars transfer missions
Fowler, W. T.↗
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Results for “GUIDANCE AND CONTROL”
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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Introduction
Saturn launch vehicle configurations, stages, and guidance and control systems, and wind effects on vehicle design
Blair, J. C.↗
Electronics Systems SRT
Guidance and control systems, communication, data acquisition, instrumentation, and electronics techniques for space application
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Space programs summary no. 37-63, volume 3 for the period 1 April - 31 May 1970. Supporting research and advanced development
Research and development work in space sciences, telecommunications, guidance and control, engineering mechanics, astrionics, propulsion, and mission analysis
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Mariner IV revisited, or the Tale of the Ancient Mariner
Mariner 4 guidance and control system performance from mission nominal end to final termination time
Scull, J. R.↗
Display requirements for advanced manned spacecraft
Control display requirements for manned spacecraft, integrating human operator with vehicle control system and determining man machine relations in stabilization, control and guidance
Duncan, R. C.↗
Apollo crew procedures, simulation, and flight planning
Apollo crew procedures, simulation and flight planning, discussing navigation, guidance and control procedures
North, W. J.↗
A new vector-matrix second order sensitivity equation with application to entry problem
Vector-matrix differential equation for second order sensitivity coefficients applied to trajectory optimization, modeling and compensation and guidance and control
Cefola, P. J.↗
Digital flight control and landing system for the CH-46C helicopter Final report
Systems analysis of flight control and guidance of CH-46C helicopter
Cockayne, W.↗
Performance verification of the lunar descent program - P66 auto, task E-72C
Results of simulated runs to evaluate lunar module descent performance of P66 automatic control and guidance system
Dwivedi, N. P.↗
Reconfigurable G and C computer study for space station use. Volume 1 - Technical summary Final report, 29 Dec. 1969 - 31 Jan. 1971
Technical summary of reconfigurable guidance and control computer for space station application - Vol. 1
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Reconfigurable G and C computer study for space station use. Volume 2 - Final technical report Final report, 29 Dec. 1969 - 31 Jan. 1971
Design and development of reconfigurable guidance and control computer for space station applications - Vol. 2
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Reconfigurable G and C computer study for space station use. Volume 3, appendix 1 - technical report, 29 Dec. 1969 - 31 Jan. 1971
Requirements for performance of reconfigurable guidance and control computer for space station applications - Vol. 3
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Reconfigurable G and C computer study for space station use. Volume 4, appendix 2 - IOP-VCS detailed design Final report, 29 Dec. 1969 - 31 Jan. 1971
Design and development of input/output processor and voter-comparator switch concept of guidance and control computer for space stations - Vol. 4
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Reconfigurable G and C computer study for space station use. Volume 5, appendix 3 - System analysis and trade-offs Final report, 29 Dec. 1969 - 31 Jan. 1971
System analysis and computer requirements derivation of guidance and control computer for space station applications - Vol. 5
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Reconfigurable G and C computer study for space station use. Volume 6, appendix 4 - Software and simulation description and results Final report, 29 Dec. 1969 - 31 Jan. 1971
Computer programs for simulation of reconfigurable guidance and control system operation - Vol. 6
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Reconfigurable G and C computer study for space station use. Volume 7, appendix 5 - D-200 computer family. Appendix 6 - System error analysis. Appendix 7 - Reliability derivation for candidate computers. Appendix 8 - Power converter design data. Appendix 9 - Data transmission medium design Final report, 29 Dec. 1969 - 31 Jan. 1971
D-200 computer family, system error analysis, reliability derivation, and power converter design for reconfigurable guidance and control computer - Vol. 7
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Clamping assembly for inertial components Patent
Inertial component clamping assembly design for spacecraft guidance and control system mounting
Denaci, D. E.↗