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101 0 $aeng
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181   $ctxt
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183   $acr
200 00$aGuidance and control$b[electronic resource] /$fedited by Robert E. Roberson, James S. Farrior
210   $aNew York $cAcademic Press$d1962
215   $a1 online resource (686 p.)
225 1 $aProgress in astronautics and rocketry ;$vv. 8
300   $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."
311   $a1-56347-857-9 
320   $aIncludes bibliographical references and index.
327   $a""Cover""; ""Title ""; ""Copyright""; ""Guidance and Control Committee""; ""Preface""; ""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""
327   $a""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""
327   $a""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""
327   $a""H. Attitude Control""""Effects of Solar Radiation Pressure on Satellite Attitude Control""; ""Momentum Vector Considerations in Wheel-Jet Satellite Control System Design""; ""Limit Cycles in Reaction Jet Attitude Control Systems Subject to External Torques""; ""Attitude Control System Using Logically Controlled Pulses""; ""Generalized Two-Impulse Scheme for Reorienting a Spin Stabilized Vehicle""; ""Contributors to Volume 8""
410  0$aProgress in astronautics and rocketry ;$vv. 8.
606   $aSpace vehicles$xGuidance systems$vCongresses
608   $aElectronic books.
615  0$aSpace vehicles$xGuidance systems
701   $aRoberson$b Robert E$012194
701   $aFarrior$b James S$0878203
712 12$aAmerican Rocket Society Symposium$f(1961 :$eStanford, Calif.)
801  0$bMiAaPQ
801  1$bMiAaPQ
801  2$bMiAaPQ
906   $aBOOK
912   $a9910457198003321
996   $aGuidance and control$91960529
997   $aUNINA