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Guidance and control. [I] : 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

Author: Robert E Roberson; James S Farrior; American Rocket Society.
Publisher: New York : Academic Press, 1962.
Series: Progress in astronautics and rocketry, v. 8.
Edition/Format:   Print book : Conference publication : EnglishView all editions and formats
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Genre/Form: Conference papers and proceedings
Congresses
Material Type: Conference publication
Document Type: Book
All Authors / Contributors: Robert E Roberson; James S Farrior; American Rocket Society.
OCLC Number: 3329642
Description: xv, 670 pages : illustrations ; 24 cm.
Contents: 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.
Series Title: Progress in astronautics and rocketry, v. 8.
Responsibility: edited by Robert E. Roberson [and] James S. Farrior.

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