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SCIDIR_ocn774285645 |
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OCoLC |
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20231117044702.0 |
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771010s1964 nyua ob 100 0 eng d |
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|a E7B
|b eng
|e pn
|c E7B
|d OPELS
|d OCLCO
|d OCLCQ
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|a 735537327
|a 922978747
|a 961688032
|a 962721898
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|a 9781600862687
|q (e-book)
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|a 1600862683
|q (e-book)
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|a 9780123955876
|q (electronic bk.)
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|a 0123955874
|q (electronic bk.)
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|z 9781563478628
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|a (OCoLC)774285645
|z (OCoLC)735537327
|z (OCoLC)922978747
|z (OCoLC)961688032
|z (OCoLC)962721898
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|a dlr
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|a TL3250
|b .A44 1963eb
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|a 629.43/3
|2 23
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|a American Institute of Aeronautics and Astronautics Guidance and Control Conference
|d (1963 :
|c Cambridge, Mass.)
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1 |
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|a Guidance and control - II :
|b a selection of technical papers based mainly on the American Institute of Aeronautics and Astronautics Guidance and Control Conference held at Cambridge, Massachusetts, August 12-14, 1963 /
|c edited by Robert C. Langford, Charles J. Mundo.
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260 |
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|a New York :
|b Academic Press,
|c 1964.
|
300 |
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|a 1 online resource (xv, 997 pages) :
|b illustrations
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336 |
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|a text
|b txt
|2 rdacontent
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337 |
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|a computer
|b c
|2 rdamedia
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|a online resource
|b cr
|2 rdacarrier
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490 |
1 |
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|a Progress in astronautics and aeronautics ;
|v v. 13
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504 |
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|a Includes bibliographical references.
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506 |
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|3 Use copy
|f Restrictions unspecified
|2 star
|5 MiAaHDL
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533 |
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|a Electronic reproduction.
|b [Place of publication not identified] :
|c HathiTrust Digital Library,
|d 2011.
|5 MiAaHDL
|
538 |
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|a Master and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002.
|u http://purl.oclc.org/DLF/benchrepro0212
|5 MiAaHDL
|
583 |
1 |
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|a digitized
|c 2011
|h HathiTrust Digital Library
|l committed to preserve
|2 pda
|5 MiAaHDL
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|a Cover -- Title -- Copyright -- The Guidance and Control Committee -- Preface -- Contents -- I. Active and Passive Attitude Control for Space Vehicles -- An Introduction to Section on Attitude Control -- Current Status of Progress in Attitude Control -- A System for Passive Gravity-Gradient Stabilization of Earth Satellites -- Theoretical and Practical Aspects of Solar Pressure Attitude Control for Interplanetary Spacecraft -- Control Moment Gyro Gravity Stabilization -- Applications of Gyro stabilizers to Satellite Attitude Control
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|a Integral Pulse Frequency On-Off ControlA Time Optimal Attitude Control System Designed to Overcome Certain Sensor Imperfections -- Two-Pulse Attitude Control of an Asymmetric Spinning Satellite -- Bank Angle Control System for a Spinning Satellite -- Several Linear Stabilization and Reorientation Control System Configurations for a Rotating, Manned Orbital Space Station -- II. Inertial Guidance for Space Flight -- Drift of a Stable Platform Caused by Gyro Rotor Unbalance -- Stellar Alignment of a Gyroscopically Stabilized Platform during Free-Fall
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505 |
8 |
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|a Navigation and Guidance Systems Employing a Gimballess IMURigid Body Dynamics -- Stable Platform Isolation Systems -- Interrogation of Spherical-Rotor Free Gyros -- III. Onboard Techniques for Interplanetary Flight -- Background and Requirements on Radar Sensors for Spacecraft -- Stellar Techniques for Midcourse Navigation Guidance -- Infrared Horizon Sensor Techniques for Lunar and Planetary Approaches -- Novel Solar System Compasses for Interplanetary Flight -- IV. Manned Control of Space Vehicles -- Pilot-Vehicle Control System Analysis
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8 |
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|a A Survey of the Development of Models for the Human ControllerSome Predictive Characteristics of the Human Controller -- V. Deep Space Guidance and Navigation -- Discussion of Guidance Policies for Multiple-Impulse Correction of the Trajectory of a Spacecraft -- A Class of Unified Explicit Methods for Steering Throttle able and Fixed-Thrust Rockets -- New Investigations in the Field of Error Propagation -- Theory of Error Compensation in Astro-Inertial Guidance Systems for Low-Thrust Space Missions -- Statistical Filtering of Space Navigation Measurements
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|a VI. RendezvousSurvey of Rendezvous Progress -- Fuel Optimization in Orbital Rendezvous -- Guidance System Complexity vs Fuel Consumption for Midcourse Correction of Rendezvous -- Application of Pontryagin's Maximum Principle to the Lunar Orbit Rendezvous Problem -- Guidance Dynamics for the Terminal Phase of Rendezvous -- VII. Re-Entry and Landing -- A Look at the Re-Entry Problem -- A Simple Re-Entry Guidance System -- A Minimum Fuel Vertical Touchdown Lunar Landing Guidance Technique -- Contributors to Volume 13
|
650 |
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0 |
|a Space vehicles
|x Guidance systems
|v Congresses.
|
650 |
|
6 |
|a V�ehicules spatiaux
|0 (CaQQLa)201-0002510
|x Syst�emes de guidage
|0 (CaQQLa)201-0002510
|v Congr�es.
|0 (CaQQLa)201-0378219
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650 |
|
7 |
|a Space vehicles
|x Guidance systems
|2 fast
|0 (OCoLC)fst01128023
|
650 |
|
7 |
|a V�ehicules spatiaux
|x Syst�emes de commande
|x Congr�es.
|2 ram
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655 |
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2 |
|a Congress
|0 (DNLM)D016423
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655 |
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7 |
|a proceedings (reports)
|2 aat
|0 (CStmoGRI)aatgf300027316
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655 |
|
7 |
|a Conference papers and proceedings
|2 fast
|0 (OCoLC)fst01423772
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655 |
|
7 |
|a Conference papers and proceedings.
|2 lcgft
|
655 |
|
7 |
|a Actes de congr�es.
|2 rvmgf
|0 (CaQQLa)RVMGF-000001049
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700 |
1 |
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|a Langford, Robert C.
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700 |
1 |
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|a Mundo, Charles J.
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710 |
2 |
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|a American Institute of Aeronautics and Astronautics.
|
776 |
0 |
8 |
|i Print version:
|a American Institute of Aeronautics and Astronautics Guidance and Control Conference (1963 : Cambridge, Mass.).
|t Guidance and control - II.
|d New York : Academic Press, 1964
|w (DLC) 62013119
|
830 |
|
0 |
|a Progress in astronautics and aeronautics ;
|v v. 13.
|
856 |
4 |
0 |
|u https://sciencedirect.uam.elogim.com/science/book/9780123955876
|z Texto completo
|