Citation: Kc. Howell et al., APPLICATION OF DYNAMICAL-SYSTEMS THEORY TO TRAJECTORY DESIGN FOR A LIBRATION POINT MISSION, The Journal of the astronautical sciences, 45(2), 1997, pp. 161-178
Citation: J. Pelaez et al., STRATEGIES FOR MAXIMIZING A SATELLITE LIFETIME BY TETHER-MEDIATED ORBITAL INJECTION, The Journal of the astronautical sciences, 45(2), 1997, pp. 205-231
Citation: Pl. Vergez, LYAPUNOV STABILITY ANALYSIS OF AN ORBIT DETERMINATION PROBLEM, The Journal of the astronautical sciences, 45(2), 1997, pp. 233-245
Citation: D. Mortari, ENERGY APPROACH ALGORITHM FOR ATTITUDE DETERMINATION FROM VECTOR OBSERVATIONS, The Journal of the astronautical sciences, 45(1), 1997, pp. 41-55
Citation: Aj. Ericssonjackson et al., ACTUATOR SENSOR PLACEMENT USING DEGREE OF CONTROLLABILITY AND OBSERVABILITY FOR DIGITALLY CONTROLLED ORBITING PLATFORMS/, The Journal of the astronautical sciences, 45(1), 1997, pp. 73-89
Citation: Y. Kim et al., NEAR-MINIMUM-TIME CONTROL OF SMART STRUCTURES FOR SLEW MANEUVER, The Journal of the astronautical sciences, 45(1), 1997, pp. 91-111
Authors:
ROWLANDS DD
LUTHCKE SB
MARSHALL JA
COX CM
WILLIAMSON RG
ROWTON SC
Citation: Dd. Rowlands et al., SPACE-SHUTTLE PRECISION ORBIT DETERMINATION IN SUPPORT OF SLA-1 USINGTDRSS AND GPS TRACKING DATA, The Journal of the astronautical sciences, 45(1), 1997, pp. 113-129
Citation: S. Djerassi, DYNAMICS OF A SATELLITE RETRACTING A LONG ELASTIC APPENDAGE, The Journal of the astronautical sciences, 44(4), 1996, pp. 425-442
Citation: H. Schaub et al., GLOBALLY STABLE FEEDBACK LAWS FOR NEAR-MINIMUM-FUEL AND NEAR-MINIMUM-TIME POINTING MANEUVERS FOR A LANDMARK-TRACKING SPACECRAFT, The Journal of the astronautical sciences, 44(4), 1996, pp. 443-466
Citation: C. Sabol et al., REFINEMENT OF A SUN-SYNCHRONOUS, CRITICALLY INCLINED ORBIT FOR THE ELLIPSO(TM) PERSONAL COMMUNICATION-SYSTEM, The Journal of the astronautical sciences, 44(4), 1996, pp. 467-489
Citation: J. Pelaez et Ec. Lorenzini, SENSITIVITY ANALYSIS OF TETHER-MEDIATED ORBITAL INJECTION, The Journal of the astronautical sciences, 44(4), 1996, pp. 491-514
Citation: Pj. Melvin et al., THE ANALYSIS OF GPS ATTITUDE DATA FROM A SLOWLY ROTATING, SYMMETRICALGRAVITY GRADIENT SATELLITE, The Journal of the astronautical sciences, 44(4), 1996, pp. 515-539
Citation: B. Blancke et Jl. Carr, MIGRATION AND THE STATIC STABILITY OF SPINNING SPACECRAFT, The Journal of the astronautical sciences, 44(3), 1996, pp. 277-292
Authors:
BERNELLIZAZZERA F
ERCOLIFINZI A
MANTEGAZZA P
Citation: F. Bernellizazzera et al., ATTITUDE MANEUVERS OF A FLEXIBLE SPACE STATION BY MEANS OF DEPLOYABLETETHERS, The Journal of the astronautical sciences, 44(3), 1996, pp. 293-313
Citation: Pkc. Wang et Fy. Hadaegh, COORDINATION AND CONTROL OF MULTIPLE MICROSPACECRAFT MOVING IN FORMATION, The Journal of the astronautical sciences, 44(3), 1996, pp. 315-355
Citation: G. Creamer, SPACECRAFT ATTITUDE DETERMINATION USING GYROS AND QUATERNION MEASUREMENTS, The Journal of the astronautical sciences, 44(3), 1996, pp. 357-371
Citation: H. Schaub et al., ADAPTIVE EXTERNAL TORQUE ESTIMATION BY MEANS OF TRACKING A LYAPUNOV FUNCTION, The Journal of the astronautical sciences, 44(3), 1996, pp. 373-387
Citation: Dg. Tuckness et Sy. Young, INVESTIGATING STOCHASTIC OBSERVABILITY OF AN ANGLE-ONLY TRACKING FILTER, The Journal of the astronautical sciences, 44(3), 1996, pp. 389-408
Citation: Hj. Rim et al., DYNAMIC ORBIT DETERMINATION FOR THE EOS LASER ALTIMETER SATELLITE (EOS ALT GLAS) USING GPS MEASUREMENTS/, The Journal of the astronautical sciences, 44(3), 1996, pp. 409-424
Citation: Nj. Kasdin et C. Gauthier, GRAVITY GRADIENT GYROSCOPE DRIFTS IN THE NASA RELATIVITY MISSION GRAVITY PROBE-B EXPERIMENT, The Journal of the astronautical sciences, 44(2), 1996, pp. 129-147