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EBOOKCENTRAL_ocn774285667 |
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120113s1962 nyuad ob 101 0 eng d |
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|a TL3250
|b .G85 1962eb
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082 |
0 |
4 |
|a 629.43/3
|2 23
|
049 |
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|a UAMI
|
245 |
0 |
0 |
|a Guidance and control /
|c edited by Robert E. Roberson, James S. Farrior.
|
264 |
|
1 |
|a New York :
|b Academic Press,
|c 1962.
|
300 |
|
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|a 1 online resource (xv, 670 pages) :
|b illustrations
|
336 |
|
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|a text
|b txt
|2 rdacontent
|
337 |
|
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|a computer
|b c
|2 rdamedia
|
338 |
|
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|a online resource
|b cr
|2 rdacarrier
|
490 |
1 |
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|a Progress in astronautics and rocketry ;
|v v. 8
|
500 |
|
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|a "A selection of technical papers based mainly on a Symposium of the American Rocket Society held at Stanford University, Stanford, California August 7-9, 1961."
|
504 |
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|a Includes bibliographical references and index.
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505 |
0 |
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|a A. Ascent. Launch-on-Time Analysis for Space Missions ; Application of Pontryagin's Maximum Principle in Determining the Optimum Control of a Variable- Mass Vehicle ; Optimalizing Techniques for Injection Guidance -- B. Space Operations. Station Keeping of Satellites in Rendezvous Compatible Orbits ; Injection Guidance Accuracy as Applied to Lunar and Interplanetary Missions ; Techniques for Error Analysis of Trajectories ; Calculus of Perturbations Applied to Lunar Mission Analysis ; Precision Tracking of Space Vehicles -- C. Descent. Terminal Guidance System for Soft Lunar Landing ; Longitudinal Range Control for a Lifting Vehicle Entering a Planetary Atmosphere ; Automatic Re-Entry Guidance at Escape Velocity -- D. Inertial Navigation ; Application of Sideband Folding Techniques to the Navigation Satellite System ; Damping an Inertial Navigation System ; Multiple Inertial System Operation in Long Term Navigation; Fundamental Limitations on Inertial Measurements -- E. Inertial Components. The King Inertial Navigation Gyro ; Design Features of the G8 Two Degree of Freedom Floated Gyroscope ; Miniature Integrating Gyro Design ; Principles of the Electric Vacuum Gyroscope -- F. Optical Navigation ; Infrared Navigation Sensors for Space Vehicles ; Optical Doppler for Space Navigation ; Noise Consideration in Designing a Traveling Wave Tube Mixer for Optical Heterodyning -- G. Adaptive Systems ; Model Reference Adaptive Systems to Improve Reliability ; Path-Adaptive Mode for Guiding Space Flight Vehicles -- H. Attitude Control. Effects of Solar Radiation Pressure on Satellite Attitude Control ; Momentum Vector Considerations in Wheel-Jet Satellite Control System Design ; Limit Cycles in Reaction Jet Attitude Control Systems Subject to External Torques ; Attitude Control System Using Logically Controlled Pulses ; Generalized Two-Impulse Scheme for Reorienting a Spin Stabilized Vehicle.
|
590 |
|
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|a ProQuest Ebook Central
|b Ebook Central Academic Complete
|
650 |
|
0 |
|a Space vehicles
|x Guidance systems
|v Congresses.
|
650 |
|
6 |
|a Véhicules spatiaux
|x Systèmes de guidage
|v Congrès.
|
650 |
|
7 |
|a Space vehicles
|x Guidance systems
|2 fast
|
655 |
|
2 |
|a Congress
|
655 |
|
7 |
|a proceedings (reports)
|2 aat
|
655 |
|
7 |
|a Conference papers and proceedings
|2 fast
|
655 |
|
7 |
|a Conference papers and proceedings.
|2 lcgft
|
655 |
|
7 |
|a Actes de congrès.
|2 rvmgf
|
700 |
1 |
|
|a Roberson, Robert E.,
|e editor.
|
700 |
1 |
|
|a Farrior, James S.,
|e editor.
|
711 |
2 |
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|a American Rocket Society Symposium
|d (1961 :
|c Stanford, Calif.)
|j issuing body.
|
758 |
|
|
|i has work:
|a Guidance and control (Text)
|1 https://id.oclc.org/worldcat/entity/E39PCGwQg4MB6JcmRDTfGwC9fy
|4 https://id.oclc.org/worldcat/ontology/hasWork
|
776 |
0 |
8 |
|i Print version:
|t Guidance and control.
|d New York : Academic Press, 1962
|w (DLC) 62013119
|
830 |
|
0 |
|a Progress in astronautics and rocketry ;
|v v. 8.
|
856 |
4 |
0 |
|u https://ebookcentral.uam.elogim.com/lib/uam-ebooks/detail.action?docID=3111484
|z Texto completo
|
938 |
|
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|
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|a ebrary
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|a ProQuest MyiLibrary Digital eBook Collection
|b IDEB
|n cis25224887
|
938 |
|
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|a YBP Library Services
|b YANK
|n 7355897
|
994 |
|
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|a 92
|b IZTAP
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