Citation: Sy. Park et Jl. Junkins, ORBITAL MISSION ANALYSIS FOR A LUNAR MAPPING SATELLITE, The Journal of the astronautical sciences, 43(2), 1995, pp. 207-217
Citation: Pm. Bainum et Jk. Xu, CALIBRATION OF TIP POSITION DURING MANEUVERS OF SPACE-ROBOTIC SYSTEMS, The Journal of the astronautical sciences, 43(1), 1995, pp. 1-23
Citation: Jm. Longuski et P. Tsiotras, ANALYTIC SOLUTION OF THE LARGE-ANGLE PROBLEM IN RIGID-BODY ATTITUDE DYNAMICS, The Journal of the astronautical sciences, 43(1), 1995, pp. 25-46
Citation: Ap. Mazzoleni et Al. Schlack, FULL-FIELD STABILITY ANALYSIS OF GUY-WIRED SATELLITES, The Journal of the astronautical sciences, 43(1), 1995, pp. 47-57
Citation: Pj. Gage et al., INTERPLANETARY TRAJECTORY OPTIMIZATION USING A GENETIC ALGORITHM, The Journal of the astronautical sciences, 43(1), 1995, pp. 59-75
Citation: Dd. Rowlands et al., MULTIRATE NUMERICAL-INTEGRATION OF SATELLITE ORBITS FOR INCREASED COMPUTATIONAL-EFFICIENCY, The Journal of the astronautical sciences, 43(1), 1995, pp. 89-100
Citation: V. Coverstonecarroll et Sn. Williams, OPTIMAL LOW THRUST TRAJECTORIES USING DIFFERENTIAL INCLUSION CONCEPTS, The Journal of the astronautical sciences, 42(4), 1994, pp. 379-393
Citation: R. Kotaru et Pm. Bainum, ON THE DYNAMICS AND CONTROL OF AN ORBITING FLEXIBLE SHALLOW SPHERICAL-SHELL IN THE PRESENCE OF SOLAR-RADIATION, The Journal of the astronautical sciences, 42(4), 1994, pp. 395-419
Citation: Mj. Bell et Jl. Junkins, NEAR MINIMUM-TIME 3-DIMENSIONAL MANEUVERS OF RIGID AND FLEXIBLE SPACECRAFT, The Journal of the astronautical sciences, 42(4), 1994, pp. 421-438
Citation: Ak. Banerjee et Rj. Klineschoder, ATTITUDE-CONTROL OF AN ORBITING TETHERED GYROSTAT, The Journal of the astronautical sciences, 42(4), 1994, pp. 439-449
Citation: Sm. Yang et Yc. Liu, OPTIMAL OUTPUT-FEEDBACK CONTROL OF SLEWING STRUCTURES WITH SPILLOVER STABILIZATION, The Journal of the astronautical sciences, 42(4), 1994, pp. 473-485
Citation: Mk. Johnson et Da. Cicci, IMPROVEMENTS IN VENUS GRAVITY-FIELD DETERMINATION USING RIDGE-TYPE ESTIMATION METHODS, The Journal of the astronautical sciences, 42(4), 1994, pp. 487-500
Citation: Jt. Betts, OPTIMAL INTERPLANETARY ORBIT TRANSFERS BY DIRECT TRANSCRIPTION, The Journal of the astronautical sciences, 42(3), 1994, pp. 247-268
Citation: Ca. Kluever et Bl. Pierson, OPTIMAL LOW-THRUST EARTH-MOON TRANSFERS WITH A SWITCHING FUNCTION-STRUCTURE, The Journal of the astronautical sciences, 42(3), 1994, pp. 269-283
Citation: M. Keshmiri et al., EFFECTS OF AERODYNAMIC LIFT ON THE STABILITY OF TETHERED SATELLITE SYSTEMS, The Journal of the astronautical sciences, 42(3), 1994, pp. 301-318
Citation: Rz. Zhu et al., DYNAMICS AND CONTROL OF COUPLED ORBITAL AND LIBRATIONAL MOTION OF TETHERED SATELLITE SYSTEMS, The Journal of the astronautical sciences, 42(3), 1994, pp. 319-342
Citation: Zz. Tan et Pm. Bainum, THE HYBRID CONTROL OF AN ORBITING FLEXIBLE TETHERED ANTENNA REFLECTORSYSTEM, The Journal of the astronautical sciences, 42(3), 1994, pp. 343-359
Citation: Sa. Striepe et al., RADIATION EXPOSURE PREDICTIONS FOR LONG-DURATION-STAY MARS MISSIONS, The Journal of the astronautical sciences, 42(2), 1994, pp. 131-142
Citation: Dl. Hale et Mi. Cruz, INVESTIGATION OF THE FEASIBILITY OF USING A FLEXIBLE AEROBRAKE FOR MARS ENTRY, The Journal of the astronautical sciences, 42(2), 1994, pp. 153-174
Citation: Z. Li et Pm. Bainum, 3-D MANEUVER AND VIBRATION CONTROL OF FLEXIBLE SPACECRAFT USING THE MOMENTUM EXCHANGE FEEDBACK-CONTROL CONCEPT, The Journal of the astronautical sciences, 42(2), 1994, pp. 175-188