Guidance and control / edited by Robert E. Roberson, James S. Farrior.

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Bibliographic Details
Corporate Author: American Rocket Society Symposium
Other Authors: Roberson, Robert E. (Editor), Farrior, James S. (Editor)
Format: eBook
Language:English
Published: New York : Academic Press, 1962.
Series:Progress in astronautics and rocketry ; v. 8.
Subjects:
Online Access:Click for online access

MARC

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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 |a 1 online resource (xv, 670 pages) :  |b illustrations 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
490 1 |a Progress in astronautics and rocketry ;  |v v. 8 
500 |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 |a Includes bibliographical references and index. 
505 0 |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. 
650 0 |a Space vehicles  |x Guidance systems  |v Congresses. 
650 7 |a Space vehicles  |x Guidance systems  |2 fast 
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 |a American Rocket Society Symposium  |d (1961 :  |c Stanford, Calif.)  |j issuing body. 
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.proquest.com/lib/holycrosscollege-ebooks/detail.action?docID=3111484  |y Click for online access 
903 |a EBC-AC 
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