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
Citation: E. Vandoorn et Sf. Asokanthan, ATTITUDE STABILITY OF DUAL-SPIN ASYMMETRIC SPACECRAFT, The Journal of the astronautical sciences, 44(2), 1996, pp. 149-165
Citation: Ta. Ely et Kc. Howell, LONG-TERM EVOLUTION OF ARTIFICIAL-SATELLITE ORBITS DUE TO RESONANT TESSERAL HARMONICS, The Journal of the astronautical sciences, 44(2), 1996, pp. 167-190
Citation: M. Pasca et Ec. Lorenzini, OPTIMIZATION OF A LOW-ALTITUDE TETHERED PROBE FOR MARTIAN ATMOSPHERICDUST COLLECTION, The Journal of the astronautical sciences, 44(2), 1996, pp. 191-205
Citation: Sa. Striepe et Pn. Desai, PILOTED MARS MISSIONS USING CRYOGENIC AND STORABLE PROPELLANTS, The Journal of the astronautical sciences, 44(2), 1996, pp. 207-222
Citation: Jp. How et Dw. Miller, ASSESSMENT OF MODELING AND ROBUST-CONTROL TECHNIQUES FOR FUTURE SPACECRAFT - MIDDECK ACTIVE CONTROL EXPERIMENT, The Journal of the astronautical sciences, 44(2), 1996, pp. 223-240
Citation: S. Chenumalla et Sn. Singh, CONTROL OF ELASTIC SPACECRAFT BY NONLINEAR INVERSION AND SINGULAR PERTURBATION, The Journal of the astronautical sciences, 44(2), 1996, pp. 241-261
Citation: S. Kawase, BIAS-ERROR REDUCING TECHNIQUE FOR SYNCHRONOUS ORBIT DETERMINATION, The Journal of the astronautical sciences, 44(2), 1996, pp. 263-275
Citation: H. Schaub et Jl. Junkins, STEREOGRAPHIC ORIENTATION PARAMETERS FOR ATTITUDE DYNAMICS - A GENERALIZATION OF THE RODRIGUES PARAMETERS, The Journal of the astronautical sciences, 44(1), 1996, pp. 1-19
Citation: Fw. Boltz, GENERAL TRANSFORMATION OF KEPLERS EQUATION FOR P-ITERATIVE SOLUTION OF THE LAMBERT GAUSS PROBLEM/, The Journal of the astronautical sciences, 44(1), 1996, pp. 21-37
Citation: Ld. Mullins et Sw. Evans, THE DYNAMICS OF THE PROPOSED ORBIT FOR THE AXAF SATELLITE, The Journal of the astronautical sciences, 44(1), 1996, pp. 39-62
Citation: M. Palacios et C. Calvo, IDEAL FRAMES AND REGULARIZATION IN NUMERICAL ORBIT COMPUTATION, The Journal of the astronautical sciences, 44(1), 1996, pp. 63-77