Citation: Br. Hoelscher et Sr. Vadali, OPTIMAL OPEN-LOOP AND FEEDBACK-CONTROL USING SINGLE GIMBAL CONTROL MOMENT GYROSCOPES, The Journal of the astronautical sciences, 42(2), 1994, pp. 189-206
Citation: Kc. Howell et Sc. Gordon, ORBIT DETERMINATION ERROR ANALYSIS AND A STATION-KEEPING STRATEGY FORSUN-EARTH L(1) LIBRATION POINT ORBITS, The Journal of the astronautical sciences, 42(2), 1994, pp. 207-228
Citation: Ja. Marshall et Sb. Luthcke, RADIATIVE FORCE MODEL PERFORMANCE FOR TOPEX POSEIDON PRECISION ORBIT DETERMINATION/, The Journal of the astronautical sciences, 42(2), 1994, pp. 229-246
Citation: Nm. Hussain et Tr. Kane, 3-DIMENSIONAL REORIENTATION OF A SYSTEM OF INTERCONNECTED RIGID BODIES, The Journal of the astronautical sciences, 42(1), 1994, pp. 1-25
Citation: Vt. Coppola et J. Palacian, ELIMINATION OF THE LATITUDE IN ARTIFICIAL-SATELLITE THEORY, The Journal of the astronautical sciences, 42(1), 1994, pp. 27-34
Citation: Ta. Wetzel et Dd. Moerder, VEHICLE TRAJECTORY OPTIMIZATION FOR AEROCAPTURE AT MARS, The Journal of the astronautical sciences, 42(1), 1994, pp. 71-89
Citation: S. Pradhan et al., MATRIX-METHOD FOR EIGENVALUE ASSIGNMENT - THE SINGLE-INPUT CASE, The Journal of the astronautical sciences, 42(1), 1994, pp. 91-111
Citation: Ea. Medina et al., MIMO SYSTEM-IDENTIFICATION USING FREQUENCY-RESPONSE DATA, The Journal of the astronautical sciences, 42(1), 1994, pp. 113-129
Citation: Iy. Baritzhack, THE PIOGRAM - AN EASY TOOL FOR ANGULAR POSITION AND RATE COMPUTATIONS, The Journal of the astronautical sciences, 41(4), 1993, pp. 519-529
Citation: Md. Shuster et Ga. Natanson, QUATERNION COMPUTATION FROM A GEOMETRIC POINT-OF-VIEW, The Journal of the astronautical sciences, 41(4), 1993, pp. 545-556
Citation: Hs. Morton, HAMILTONIAN AND LAGRANGIAN FORMULATIONS OF RIGID-BODY ROTATIONAL-DYNAMICS BASED ON THE EULER PARAMETERS, The Journal of the astronautical sciences, 41(4), 1993, pp. 569-591
Citation: Ra. Broucke, ON THE USE OF POINCARE SURFACES OF SECTION IN RIGID-BODY MOTION, The Journal of the astronautical sciences, 41(4), 1993, pp. 593-601
Citation: Nc. Singer et Wp. Seering, 2 EXTENSIONS TO KANES METHOD FOR SIMPLIFYING EQUATION DERIVATION, The Journal of the astronautical sciences, 41(3), 1993, pp. 283-298
Citation: Jd. Vedder et al., ORBITAL DEBRIS HAZARD FOR NUCLEAR ELECTRIC PROPULSION EARTH-ESCAPE TRAJECTORIES, The Journal of the astronautical sciences, 41(3), 1993, pp. 299-317
Citation: E. Cazalahourcade, APOGEE MANEUVER STRATEGIES FOR THE INMARSAT-2 SPACECRAFT, The Journal of the astronautical sciences, 41(3), 1993, pp. 319-338
Citation: Je. Lyne et Rd. Braun, FLEXIBLE STRATEGIES FOR MANNED MARS MISSIONS USING AEROBRAKING AND NUCLEAR THERMAL PROPULSION, The Journal of the astronautical sciences, 41(3), 1993, pp. 339-347
Citation: Jt. Betts, USING SPARSE NONLINEAR-PROGRAMMING TO COMPUTE LOW THRUST ORBIT TRANSFERS, The Journal of the astronautical sciences, 41(3), 1993, pp. 349-371
Citation: Ab. Decou, ATTITUDE AND TETHER VIBRATION CONTROL IN SPINNING TETHERED TRIANGLES FOR ORBITING INTERFEROMETRY, The Journal of the astronautical sciences, 41(3), 1993, pp. 373-398