Citation: Ja. Kechichian, COPLANAR 2-IMPULSE RENDEZVOUS IN GENERAL ELLIPTIC ORBIT WITH DRAG, The Journal of the astronautical sciences, 45(4), 1997, pp. 391-409
Citation: Rd. Robinett et Gg. Parker, LEAST-SQUARES SLIDING MODE CONTROL TRACKING OF SPACECRAFT LARGE-ANGLEMANEUVERS, The Journal of the astronautical sciences, 45(4), 1997, pp. 433-450
Citation: Gw. Davis et al., THE ACCURACY ASSESSMENT OF PRECISE ORBITS COMPUTED FROM DOPPLER TRACKING DATA, The Journal of the astronautical sciences, 45(4), 1997, pp. 451-469
Citation: Ca. Kluever, OPTIMAL LOW-THRUST INTERPLANETARY TRAJECTORIES BY DIRECT METHOD TECHNIQUES, The Journal of the astronautical sciences, 45(3), 1997, pp. 247-262
Citation: Sa. Kessler et Da. Cicci, FILTERING METHODS FOR THE ORBIT DETERMINATION OF A TETHERED SATELLITE, The Journal of the astronautical sciences, 45(3), 1997, pp. 263-278
Citation: Jl. Junkins et H. Schaub, AN INSTANTANEOUS EIGENSTRUCTURE QUASIVELOCITY FORMULATION FOR NONLINEAR MULTIBODY DYNAMICS, The Journal of the astronautical sciences, 45(3), 1997, pp. 279-295
Citation: Jr. Carpenter et Rh. Bishop, FLIGHT-DATA RESULTS OF ESTIMATE FUSION FOR SPACECRAFT RENDEZVOUS NAVIGATION FROM SHUTTLE MISSION STS-69, The Journal of the astronautical sciences, 45(3), 1997, pp. 297-319
Citation: Dm. Ma et al., ANALYTIC THEORY OF OPTIMAL PLANE CHANGE BY LOW AERODYNAMIC FORCES, The Journal of the astronautical sciences, 45(3), 1997, pp. 329-347
Authors:
LUTHCKE SB
MARSHALL JA
ROWTON SC
RACHLIN KE
COX CM
WILLIAMSON RG
Citation: Sb. Luthcke et al., ENHANCED RADIATIVE FORCE MODELING OF THE TRACKING AND DATA RELAY SATELLITES, The Journal of the astronautical sciences, 45(3), 1997, pp. 349-370
Authors:
CHAO CC
GUNNING GR
MOE K
CHASTAIN SH
SETTECERRI TJ
Citation: Cc. Chao et al., AN EVALUATION OF JACCHIA-71 AND MSIS90 ATMOSPHERE MODELS WITH NASA ODERACS DECAY DATA, The Journal of the astronautical sciences, 45(2), 1997, pp. 131-141
Citation: Sn. Williams et V. Coverstonecarroll, BENEFITS OF SOLAR ELECTRIC PROPULSION FOR THE NEXT-GENERATION OF PLANETARY EXPLORATION MISSIONS, The Journal of the astronautical sciences, 45(2), 1997, pp. 143-159
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