Guidance and Control

Content: 
Progress in ASTRONAUTICS and ROCKETRY, Page ii
Front Matter, Page iii
Copyright, Page iv
AMERICAN ROCKET SOCIETY, Page v
PREFACE, Pages vii-xi, Robert E. Roberson, James S. Farrior
LAUNCH-ON-TIME ANALYSIS FOR SPACE MISSIONS, Pages 3-20, C.E. Kohlhase
APPLICATION OF PONTRYAGIN'S MAXIMUM PRINCIPLE IN DETERMINING THE OPTIMUM CONTROL OF A VARIABLE-MASS VEHICLE, Pages 21-29, Dahlard Lukes
OPTIMALIZING TECHNIQUES FOR INJECTION GUIDANCE, Pages 31-54, Wayne Schmaedeke, George Swanlund
STATION KEEPING OF SATELLITES IN RENDEZVOUS COMPATIBLE ORBITS, Pages 57-87, Robert S. Swanson, Peter W. Soule, Norman V. Petersen
INJECTION GUIDANCE ACCURACY AS APPLIED TO LUNAR AND INTERPLANETARY MISSIONS, Pages 89-124, H.J. Gordon
TECHNIQUES FOR ERROR ANALYSIS OF TRAJECTORIES, Pages 125-146, Arnold Peske, Michael Ward
CALCULUS OF PERTURBATIONS APPLIED TO LUNAR MISSION ANALYSIS, Pages 147-194, William C. Marshall
PRECISION TRACKING OF SPACE VEHICLES, Pages 195-213, C.R. Woods, E.B. Mullen
TERMINAL GUIDANCE SYSTEM FOR SOFT LUNAR LANDING, Pages 217-239, R.K. Cheng, I. Pfeffer
LONGITUDINAL RANGE CONTROL FOR A LIFTING VEHICLE ENTERING A PLANETARY ATMOSPHERE, Pages 241-270, Richard Rosenbaum
AUTOMATIC RE-ENTRY GUIDANCE AT ESCAPE VELOCITY, Pages 271-308, Paul C. Dow Jr., Donald P. Fields, Frank H. Scammell
APPLICATION OF SIDEBAND FOLDING TECHNIQUES TO THE NAVIGATION SATELLITE SYSTEM, Pages 311-324, James W. Crooks Jr., Robert C. Weaver, Malvin M. Cox
DAMPING AN INERTIAL NAVIGATION SYSTEM, Pages 325-348, Charles Broxmeyer
MULTIPLE INERTIAL SYSTEM OPERATION IN LONG TERM NAVIGATION, Pages 349-366, Richard R. Palmer, Donald F. McAllister
FUNDAMENTAL LIMITATIONS ON INERTIAL MEASUREMENTS, Pages 367-394, Myron Kayton
THE KING INERTIAL NAVIGATION GYRO, Pages 397-410, Clifford O. Swanson
DESIGN FEATURES OF THE G8 TWO DEGREE OF FREEDOM FLOATED GYROSCOPE, Pages 411-420, Sidney Osband
MINIATURE INTEGRATING GYRO DESIGN, Pages 421-434, Roger P. Durkee
PRINCIPLES OF THE ELECTRIC VACUUM GYROSCOPE, Pages 435-440, A. Nordsieck
INFRARED NAVIGATION SENSORS FOR SPACE VEHICLES, Pages 443-468, Eric M. Wormser, Morris H. Arck
OPTICAL DOPPLER FOR SPACE NAVIGATION, Pages 469-486, R.G. Franklin, D.L. Birx
NOISE CONSIDERATION IN DESIGNING A TRAVELING WAVE TUBE MIXER FOR OPTICAL HETERODYNING, Pages 487-496, W.C. Reisener Jr.
MODEL REFERENCE ADAPTIVE SYSTEMS TO IMPROVE RELIABILITY, Pages 499-522, H.P. Whitaker, Allen Kezer
PATH-ADAPTIVE MODE FOR GUIDING SPACE FLIGHT VEHICLES, Pages 523-540, W.E. Miner, D.H. Schmieder, N.J. Braud
EFFECTS OF SOLAR RADIATION PRESSURE ON SATELLITE ATTITUDE CONTROL, Pages 543-564, R.J. McElvain
MOMENTUM VECTOR CONSIDERATIONS IN WHEEL-JET SATELLITE CONTROL SYSTEM DESIGN, Pages 565-597, D.B. DeBra, R.H. Cannon Jr.
LIMIT CYCLES IN REACTION JET ATTITUDE CONTROL SYSTEMS SUBJECT TO EXTERNAL TORQUES, Pages 599-627, P.R. Dahl, G.T. Aldrich, L.K. Herman
ATTITUDE CONTROL SYSTEM USING LOGICALLY CONTROLLED PULSES, Pages 629-648, R.S. Gaylord, W.N. Keller
GENERALIZED TWO-IMPULSE SCHEME FOR REORIENTING A SPIN STABILIZED VEHICLE, Pages 649-668, Carl Grubin
CONTRIBUTORS TO VOLUME 8, Pages 669-670