CURRENT STATUS OF PROGRESS IN ATTITUDE CONTROL

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[3]  M. J. Abzug,et al.  A TIME OPTIMAL ATTITUDE CONTROL SYSTEM DESIGNED TO OVERCOME CERTAIN SENSOR IMPERFECTIONS , 1963 .

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[6]  J. G. Bland,et al.  Simply mechanized attitude control for spinning vehicles , 1963 .

[7]  P. C. Wheeler,et al.  TWO-PULSE ATTITUDE CONTROL OF AN ASYMMETRIC SPINNING SATELLITE; APPENDIX - EFFECT OF NODAL REGRESSION UPON BANK AND YAW ERROR , 1963 .

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[10]  Henry Reid,et al.  MINIGUIDE - A SIMPLIFIED ATTITUDE CONTROL FOR SPINSTABILIZED VEHICLES , 1963 .

[11]  H. Tuchyner.  OPTIMIZATION OF A MERCURY REACTION FLYWHEEL SYSTEM FOR THREE-AXIS ATTITUDE CONTROL , 1963 .

[12]  K. Magnus.  Rotational motions of satellites in a radial gravity field , 1963 .

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[14]  Walter Haeussermann,et al.  Recent Advances in Attitude Control of Space Vehicles , 1962 .

[15]  E.G.C. Burt,et al.  On the attitude control of earth satellites , 1962 .

[16]  John S. White,et al.  STUDY OF A SATELLITE ATTITUDE CONTROL SYSTEM USING INTEGRATING GYROS AS TORQUE SOURCES , 1961 .

[17]  John S. White,et al.  Satellite Attitude Control Utilizing the Earth's Magnetic Field , 1961 .

[18]  John S. White,et al.  Study of Systems Using Inertia Wheels for Precise Attitude Control of a Satellite , 1961 .

[19]  R. H. Cannon,et al.  Basic response relations for space vehicle attitude control using gyros. , 1965 .

[20]  Robert J. Mcelvain,et al.  Satellite Angular Momentum Removal Utilizing the Earth's Magnetic Field , 1964 .

[21]  A. E. Sabroff,et al.  INTEGRAL PULSE FREQUENCY ON-OFF CONTROL , 1964 .

[22]  Robert E. Roberson,et al.  Dynamical model for fine pointing attitude control of the Orbiting Astronomical Observatory , 1963 .

[23]  J. Braumiller,et al.  MAGNETIC TORQUERS FOR SPACE VEHICLE CONTROL , 1963 .

[24]  J. Nicklas,et al.  THEORETICAL AND PRACTICAL ASPECTS OF SOLAR PRESSURE ATTITUDE CONTROL FOR INTERPLANETARY SPACECRAFT , 1963 .

[25]  R. S. Gaylord,et al.  ATTITUDE CONTROL SYSTEM USING LOGICALLY CONTROLLED PULSES , 1962 .

[26]  R. H. Cannon,et al.  MOMENTUM VECTOR CONSIDERATIONS IN WHEEL-JET SATELLITE CONTROL SYSTEM DESIGN , 1962 .