<title>Author Index</title>
<h1> 1995 AAS/AIAA Astrodynamics Specialists Conference Author Index</h1>
<dl>
<dt>Abusali, P. A. M.	 
<dd><a href="abstracts/96-180.html"><b>STS-69 RELATIVE POSITIONING GPS EXPERIMENT</b></a>

<dt>Abusali, P. A. M. 	 
<dd><a href="abstracts/96-186.html"><b>AUTONOMOUS NAVIGATION OF BLOCK II-R GPS SATELLITE USING CROSS-LINK MEASUREMENTS</b></a>

<dt>Andrews, S. E. 	 
<dd><a href="abstracts/96-116.html"><b>SIGNATURE ANALYSIS OF DEBRIS FROM THE 1994 AIR FORCE SPACE COMMAND DEBRIS CAMPAIGN</b></a>

<dt>Anz-Meador, P. 	 
<dd><a href="abstracts/96-115.html"><b>A NEW AND DETAILED EVALUATION OF THE NUMBER AND MASSES OF OBJECTS IN EARTH ORBIT</b></a>

<dt>Anzenhofer, M. 	 
<dd><a href="abstracts/96-164.html"><b>CROSS-CALIBRATION OF ERS-2 RADAR ALTIMETER USING PRECISION ERS ORBITS</b></a>

<dt>Asokanthan, S. F. 	 
<dd><a href="abstracts/96-159.html"><b>NONLINEAR INSTABILITIES IN A DUAL-SPIN SPACECRAFT WITH AN AXIAL NUTATIONAL DAMPER</b></a>

<dt>Axelrad, P. 	 
<dd><a href="abstracts/96-143.html"><b>APPLICATION OF THE EXTENDED KALMAN FILTER FOR RELATIVE NAVIGATION IN AN ELLIPTICAL ORBIT</b></a>

<dt>Axelrad, P. 	 
<dd><a href="abstracts/96-185.html"><b>PRECISION ORBIT DETERMINATION FOR GFO AND GFO-2</b></a>

<dt>Baccus, R. 	 
<dd><a href="abstracts/96-191.html"><b>DEMONSTRATING LUNAR OXYGEN PRODUCTION:  THE TEXAS INTERDISCIPLENARY STUDENT MISSION DESIGN PROJECT</b></a>

<dt>Bahrami, K. A. 	 
<dd><a href="abstracts/96-177.html"><b>ON IMPROVING THE GALILEO SCAN PLATFORM CONE CONTROLLER PERFORMANCE IN CRUISE MODE REMOTE SENSING</b></a>

<dt>Bainum, P. M.  	 
<dd><a href="abstracts/96-162.html"><b>DEVELOPMENT OF ROBUST REDUCED ORDERED DIGITAL CONTROLLER FOR LARGE ORBITING PLATFORMS IN DISCRETE-TIME DOMAIN</b></a>

<dt>Bang, H.  	 
<dd><a href="abstracts/96-216.html"><b>CONTROL LAW DESIGN FOR AUTONOMOUS STATION COLLOCATION OF SATELLITES</b></a>

<dt>Barker, W. N. 	 
<dd><a href="abstracts/96-124.html"><b>EARTH GRAVITATIONAL ERROR BUDGET</b></a>

<dt>Bishop, R. H. 	 
<dd><a href="abstracts/96-152.html"><b>ADAPTIVE ORBIT DETERMINATION FOR INTERPLANETARY SPACECRAFT</b></a>

<dt>Bishop, R. H. 	 
<dd><a href="abstracts/96-181.html"><b>FLIGHT DATA RESULTS OF ESTIMATE FUSION FOR SPACECRAFT RENDEZVOUS NAVIGATION FROM SHUTTLE MISSION STS-69</b></a>

<dt>Bishop, R. H.  	 
<dd><a href="abstracts/96-110.html"><b>DERIVATION AND OPTIMALITY OF DISTRIBUTED FILTERING ALGORITHMS BASED ON MINIMUM VARIANCE METHODS</b></a>

<dt>Bond, V. R. 	 
<dd><a href="abstracts/96-155.html"><b>SPHERE-OF-INFLUENCE TO PLANET-FIXED COORDINATES TARGETING</b></a>

<dt>Bond, V. R. 	 
<dd><a href="abstracts/96-178.html"><b>A VARIATION OF PARAMETERS APPROACH FOR THE SOLUTION OF THE DIFFERENTIAL EQUATIONS FOR THE ROTATIONAL MOTION OF A RIGID BODY</b></a>

<dt>Born, G. H. 	 
<dd><a href="abstracts/96-108.html"><b>A NEW CLASS OF ADAPTIVE, EXTENDED KALMAN FILTER</b></a>

<dt>Born, G. H. 	 
<dd><a href="abstracts/96-185.html"><b>PRECISION ORBIT DETERMINATION FOR GFO AND GFO-2</b></a>

<dt>Brazzel, J. 	 
<dd><a href="abstracts/96-182.html"><b>FLIGHT TEST RESULTS FROM REAL-TIME RELATIVE GPS FLIGHT EXPERIMENT ON STS-69</b></a>

<dt>Burkhart, P. D. 	 
<dd><a href="abstracts/96-168.html"><b>ADVANCED LAUNCH SYSTEM TRAJECTORY OPTIMIZATION</b></a>

<dt>Burkhart, P. D.  	 
<dd><a href="abstracts/96-152.html"><b>ADAPTIVE ORBIT DETERMINATION FOR INTERPLANETARY SPACECRAFT</b></a>

<dt>Burnham, W. F. 	 
<dd><a href="abstracts/96-214.html"><b>GEOSYNCHRONOUS SURVEILLANCE WITH A SPACE-BASED SENSOR</b></a>

<dt>Campbell, D. R.	 
<dd><a href="abstracts/96-219.html"><b>CHAOTIC DYNAMICS IN A SPACECRAFT WITH A FLEXIBLE APPENDAGE AND WITH ENERGY DISSIPATION VIA A NONLINEAR CONTROLLER</b></a>

<dt>Campbell, W. S. 	 
<dd><a href="abstracts/96-112.html"><b>DEVELOPMENT OF DOD DEBRIS MITIGATION GUIDELINES</b></a>

<dt>Cant, A. 	 
<dd><a href="abstracts/96-113.html"><b>INTRODUCING IDES: CHARACTERISING THE ORBITAL DEBRIS ENVIRONMENT IN THE PAST, PRESENT, AND FUTURE</b></a>

<dt>Canu, C.	 
<dd><a href="abstracts/96-141.html"><b>EVALUATION OF THE SHUTTLE ORBIT CONTROL ACCURACY DURING THE SIR-C/X-SAR MISSION</b></a>

<dt>Carlini, S. 	 
<dd><a href="abstracts/96-213.html"><b>INTER-SATELLITE TRACKING FOR CO-LOCATION</b></a>

<dt>Carpenter, J. R. 	 
<dd><a href="abstracts/96-110.html"><b>DERIVATION AND OPTIMALITY OF DISTRIBUTED FILTERING ALGORITHMS BASED ON MINIMUM VARIANCE METHODS</b></a>

<dt>Carpenter, J. R. 	 
<dd><a href="abstracts/96-181.html"><b>FLIGHT DATA RESULTS OF ESTIMATE FUSION FOR SPACECRAFT RENDEZVOUS NAVIGATION FROM SHUTTLE MISSION STS-69</b></a>

<dt>Carpenter, R.  	 
<dd><a href="abstracts/96-182.html"><b>FLIGHT TEST RESULTS FROM REAL-TIME RELATIVE GPS FLIGHT EXPERIMENT ON STS-69</b></a>

<dt>Carter, T. E. 	 
<dd><a href="abstracts/96-199.html"><b>SHELLS OF MULTIPLE THRUST IN POWER-LIMITED RENDEZVOUS OF A SPACECRAFT</b></a>

<dt>Casali, S. J. 	 
<dd><a href="abstracts/96-124.html"><b>EARTH GRAVITATIONAL ERROR BUDGET</b></a>

<dt>Casalino, L.  	 
<dd><a href="abstracts/96-169.html"><b>INDIRECT APPROACH FOR MINIMUM-FUEL AEROASSISTED TRANSFERS</b></a>

<dt>Cefola, P. J.  	 
<dd><a href="abstracts/96-142.html"><b>THE INCLUSION OF THE NAVAL SPACE COMMAND SATELLITE THEORY PPT2 IN THE R&D GTDS ORBIT DETERMINATION SYSTEM</b></a>

<dt>Chang, K. 	 
<dd><a href="abstracts/96-100.html"><b>Approximate Solutions for Lunar Trajectory and Vehicle Optimization Using Electric PropULsion</b></a>

<dt>Chao, C. C. 	 
<dd><a href="abstracts/96-127.html"><b>AN EVALUATION OF JACCHIA 71 AND MSIS90 ATMOSPHERIC MODELS WITH NASA ODERACS DECAY DATA</b></a>

<dt>Cheng, M. 	 
<dd><a href="abstracts/96-128.html"><b>MODELING SURFACE FORCES ON THE GEODETIC SATELLITE, AJISAI</b></a>

<dt>Cheng, Y-M 	 
<dd><a href="abstracts/96-147.html"><b>DYNAMICS AND ORBIT DETERMINATION OF TETHERED SATELLITE SYSTEMS</b></a>

<dt>Cho, S. 	 
<dd><a href="abstracts/96-147.html"><b>DYNAMICS AND ORBIT DETERMINATION OF TETHERED SATELLITE SYSTEMS</b></a>

<dt>Choe, C. J. 	 
<dd><a href="abstracts/96-206.html"><b>ESTIMATION OF ICE SHEET SURFACE ELEVATION CHANGE FROM THE EOS ALTIMETER SATELLITE (ICESAT) CROSSOVER SIMULATION</b></a>

<dt>Chuba, W. A. 	 
<dd><a href="abstracts/96-148.html"><b>RELATIVISTIC ORBIT DETERMINATION</b></a>

<dt>Cicci, D. A. 	 
<dd><a href="abstracts/96-147.html"><b>DYNAMICS AND ORBIT DETERMINATION OF TETHERED SATELLITE SYSTEMS</b></a>

<dt>Cicci, D. A. 	 
<dd><a href="abstracts/96-156.html"><b>IMPROVEMENTS IN MARS GRAVITY FIELD DETERMINATION USING RIDGE-TYPE ESTIMATION METHODS</b></a>

<dt>Cochran, J. E. 	 
<dd><a href="abstracts/96-147.html"><b>DYNAMICS AND ORBIT DETERMINATION OF TETHERED SATELLITE SYSTEMS</b></a>

<dt>Coffey, S. 	 
<dd><a href="abstracts/96-125.html"><b>COMPRESSION OF SATELLITE ORBITS</b></a>

<dt>Coffey, S. L. 	 
<dd><a href="abstracts/96-146.html"><b>PARALLEL PROCESSING OF UNCORRELATED OBSERVATIONS INTO SATELLITE ORBITS</b></a>

<dt>Cohen, A. 	 
<dd><a href="abstracts/96-191.html"><b>DEMONSTRATING LUNAR OXYGEN PRODUCTION:  THE TEXAS INTERDISCIPLENARY STUDENT MISSION DESIGN PROJECT</b></a>

<dt>Colasurdo, G. 	 
<dd><a href="abstracts/96-169.html"><b>INDIRECT APPROACH FOR MINIMUM-FUEL AEROASSISTED TRANSFERS</b></a>

<dt>Conway, B. A. 	 
<dd><a href="abstracts/96-101.html"><b>OPTIMAL, LOW-THRUST, EARTH-MOON ORBIT TRANSFERS</b></a>

<dt>Conway, B. A. 	 
<dd><a href="abstracts/96-195.html"><b>OPTIMAL LOW-THRUST INTERCEPTION OF EARTH-CROSSING ASTEROIDS</b></a>

<dt>Crassidis, J. L. 	 
<dd><a href="abstracts/96-174.html"><b>PREDICITIVE FILTERING FOR ATTITUDE ESTIMATION WITHOUT RATE SENSORS</b></a>

<dt>Crowther, R. 	 
<dd><a href="abstracts/96-113.html"><b>INTRODUCING IDES: CHARACTERISING THE ORBITAL DEBRIS ENVIRONMENT IN THE PAST, PRESENT, AND FUTURE</b></a>

<dt>Cruickshank, D. R.  	 
<dd><a href="abstracts/96-108.html"><b>A NEW CLASS OF ADAPTIVE, EXTENDED KALMAN FILTER</b></a>

<dt>Culp, R. D. 	 
<dd><a href="abstracts/96-114.html"><b>DETERMINATION OF THE SIZES AND MASSES OF DEBRIS OBJECTS</b></a>

<dt>Dagen, J. 	 
<dd><a href="abstracts/96-130.html"><b>STRUCTURAL INTEGRATION OF THE SPACE SHUTTLE AND MIR SPACE STATION</b></a>

<dt>Davenport, Q. 	 
<dd><a href="abstracts/96-187.html"><b>MODELING THE INTERNAL EFFECTS WITHIN A HABITABLE MODULE DUE TO A PERFORATION BY AN ORBITAL DEBRIS PARTICLE</b></a>

<dt>Davis, G. W. 	 
<dd><a href="abstracts/96-165.html"><b>GRAVITY TUNING EXPERIMENTS FOR THE PRECISE ORBIT DETERMINATION OF THE EOS ALTIMETER SATELLITE (EOS ALT/GLAS) USING THE GPS TRACKING DATA</b></a>

<dt>DeVere, G. T.  	 
<dd><a href="abstracts/96-120.html"><b>AN EXAMINATION OF THE HISTORIES OF INTERESTING DEBRIS SATELLTES</b></a>

<dt>Djerassi, S. 	 
<dd><a href="abstracts/96-163.html"><b>DYNAMICS OF A SATELLITE RETRACTING A LONG ELASTIC APPENDAGE</b></a>

<dt>Eckstein, B. 	 
<dd><a href="abstracts/96-125.html"><b>COMPRESSION OF SATELLITE ORBITS</b></a>

<dt>Eichler, P. 	 
<dd><a href="abstracts/96-115.html"><b>A NEW AND DETAILED EVALUATION OF THE NUMBER AND MASSES OF OBJECTS IN EARTH ORBIT</b></a>

<dt>Elipe, A. 	 
<dd><a href="abstracts/96-139.html"><b>FROZEN ORBITS FOR THE ZONAL MOON POTENTIAL</b></a>

<dt>Ericsson-Jackson, A. J. 	 
<dd><a href="abstracts/96-162.html"><b>DEVELOPMENT OF ROBUST REDUCED ORDERED DIGITAL CONTROLLER FOR LARGE ORBITING PLATFORMS IN DISCRETE-TIME DOMAIN</b></a>

<dt>Evans, S. W. 	 
<dd><a href="abstracts/96-203.html"><b>POST DEPLOYMENT RECONTACT ISSUES FOR THE SEDS/SEDSAT MISSION</b></a>

<dt>Fischer, M. 	 
<dd><a href="abstracts/96-191.html"><b>DEMONSTRATING LUNAR OXYGEN PRODUCTION:  THE TEXAS INTERDISCIPLENARY STUDENT MISSION DESIGN PROJECT</b></a>

<dt>Floria, L. 	 
<dd><a href="abstracts/96-136.html"><b>CANONICAL ELEMENTS FOR PERTURBED ORBITAL MOTIOIN USING AN ARBITRARY TIME PARAMETER</b></a>

<dt>Folta, D. C. 	 
<dd><a href="abstracts/96-104.html"><b>MULTIPLE LUNAR FLYBY TARGETING FOR THE WIND MISSION</b></a>

<dt>Folta, D. C. 	 
<dd><a href="abstracts/96-103.html"><b>TRAJECTORY DETERMINATION FOR A WEAKLY BOUND TRANSLUNAR TRAJECTORY</b></a>

<dt>Foni, A. 	 
<dd><a href="abstracts/96-141.html"><b>EVALUATION OF THE SHUTTLE ORBIT CONTROL ACCURACY DURING THE SIR-C/X-SAR MISSION</b></a>

<dt>Fonte, D. J. 	 
<dd><a href="abstracts/96-142.html"><b>THE INCLUSION OF THE NAVAL SPACE COMMAND SATELLITE THEORY PPT2 IN THE R&D GTDS ORBIT DETERMINATION SYSTEM</b></a>

<dt>Fowler, W. T. 	 
<dd><a href="abstracts/96-191.html"><b>DEMONSTRATING LUNAR OXYGEN PRODUCTION:  THE TEXAS INTERDISCIPLENARY STUDENT MISSION DESIGN PROJECT</b></a>

<dt>Gabor, M. J. 	 
<dd><a href="abstracts/96-166.html"><b>A SYSTEMATIC APPROACH TO THE PRECISION ORBIT DETERMINATION OF THE GEOSAT EXACT REPEAT MISSION UTILIZING TRANET DOPPLER DATA</b></a>

<dt>Gala, D. 	 
<dd><a href="abstracts/96-187.html"><b>MODELING THE INTERNAL EFFECTS WITHIN A HABITABLE MODULE DUE TO A PERFORATION BY AN ORBITAL DEBRIS PARTICLE</b></a>

<dt>Garrison, J. L. 	 
<dd><a href="abstracts/96-143.html"><b>APPLICATION OF THE EXTENDED KALMAN FILTER FOR RELATIVE NAVIGATION IN AN ELLIPTICAL ORBIT</b></a>

<dt>Gifford, K. 	 
<dd><a href="abstracts/96-171.html"><b>ATTDES - AN EXPERT SYSTEM FOR SATELLITE ATTITUDE DETERMINATION AND CONTROL</b></a>

<dt>Gill, E.  	 
<dd><a href="abstracts/96-150.html"><b>PERTURBATION FORCES ACTING ON THE ROSETTA SPACECRAFT IN A CLOSE ORBIT AROUND COMET P/WIRTANEN</b></a>

<dt>Gold, K. 	 
<dd><a href="abstracts/96-185.html"><b>PRECISION ORBIT DETERMINATION FOR GFO AND GFO-2</b></a>

<dt>Gouldman, M. W. 	 
<dd><a href="abstracts/96-183.html"><b>ORBIT ESTIMATION RESULTS FOR TOPEX/POSEIDON BASED ON GPS TRACKING DATA</b></a>

<dt>Gravseth, I. J. 	 
<dd><a href="abstracts/96-114.html"><b>DETERMINATION OF THE SIZES AND MASSES OF DEBRIS OBJECTS</b></a>

<dt>Gray, G. L.	 
<dd><a href="abstracts/96-219.html"><b>CHAOTIC DYNAMICS IN A SPACECRAFT WITH A FLEXIBLE APPENDAGE AND WITH ENERGY DISSIPATION VIA A NONLINEAR CONTROLLER</b></a>

<dt>Graziani, F. 	 
<dd><a href="abstracts/96-170.html"><b>OPTIMAL DESCENT TRAJECTORIES FOR SCIENTIFIC PAYLOADS USING ICBM-CONVERTED LAUNCHERS</b></a>

<dt>Gruber, T. 	 
<dd><a href="abstracts/96-164.html"><b>CROSS-CALIBRATION OF ERS-2 RADAR ALTIMETER USING PRECISION ERS ORBITS</b></a>

<dt>Guinn, J. R. 	 
<dd><a href="abstracts/96-184.html"><b>GPS AUTONOMOUS NAVIGATION FOR GROUNDTRACK REPEAT ORBITS</b></a>

<dt>Gunning, G.R. 	 
<dd><a href="abstracts/96-127.html"><b>AN EVALUATION OF JACCHIA 71 AND MSIS90 ATMOSPHERIC MODELS WITH NASA ODERACS DECAY DATA</b></a>

<dt>Hall, C. D. 	 
<dd><a href="abstracts/96-197.html"><b>OPTIMAL CONTINUOUS THRUST ORBIT TRANSFERS</b></a>

<dt>Hanson, D. 	 
<dd><a href="abstracts/96-131.html"><b>SHUTTLE STABILITY AND CONTROL OF THE STS-71 SHUTTLE/MIR MATED CONFIGURATION</b></a>

<dt>Harigae, M. 	 
<dd><a href="abstracts/96-179.html"><b>ORBIT DETERMINATION OF THE ORBITAL RE-ENTRY EXPERIMENT (OREX) SPACECRAFT BY GPS</b></a>

<dt>Harigae, M. 	 
<dd><a href="abstracts/96-209.html"><b>ON THE INERTIAL MEASUREMENT UNIT USING FIBER OPTIC GYROSCOPES</b></a>

<dt>Hauptman, S. 	 
<dd><a href="abstracts/96-113.html"><b>INTRODUCING IDES: CHARACTERISING THE ORBITAL DEBRIS ENVIRONMENT IN THE PAST, PRESENT, AND FUTURE</b></a>

<dt>Hayami, R. A. 	 
<dd><a href="abstracts/96-187.html"><b>MODELING THE INTERNAL EFFECTS WITHIN A HABITABLE MODULE DUE TO A PERFORATION BY AN ORBITAL DEBRIS PARTICLE</b></a>

<dt>Herman, A. L. 	 
<dd><a href="abstracts/96-101.html"><b>OPTIMAL, LOW-THRUST, EARTH-MOON ORBIT TRANSFERS</b></a>

<dt>Hilbert, K. B. 	 
<dd><a href="abstracts/96-177.html"><b>ON IMPROVING THE GALILEO SCAN PLATFORM CONE CONTROLLER PERFORMANCE IN CRUISE MODE REMOTE SENSING</b></a>

<dt>Hinkel, H. 	 
<dd><a href="abstracts/96-182.html"><b>FLIGHT TEST RESULTS FROM REAL-TIME RELATIVE GPS FLIGHT EXPERIMENT ON STS-69</b></a>

<dt>Horta, L. 	 
<dd><a href="abstracts/96-189.html"><b>ON-ORBIT APPLICATION OF H-INFINITY TO THE MIDDECK ACTIVE CONTROLS EXPERIMENT</b></a>

<dt>Horton, W. T. 	 
<dd><a href="abstracts/96-193.html"><b>DRACO, A DEMONSTRATION AND RESEARCH GAS CAN ORBITER FOR ADVANCED TECHNOLOGY DEMONSTRATION IN LOW EARTH ORBIT</b></a>

<dt>Hui, Y. 	 
<dd><a href="abstracts/96-157.html"><b>DYNAMIC STABILITY CRITERION OF A SLOW SPIN RE-ENTRY VEHICLE</b></a>

<dt>Hujsak, R. S. 	 
<dd><a href="abstracts/96-123.html"><b>INTERPOLATED GRAVITY ACCELERATIONS</b></a>

<dt>Hull, D. G. 	 
<dd><a href="abstracts/96-168.html"><b>ADVANCED LAUNCH SYSTEM TRAJECTORY OPTIMIZATION</b></a>

<dt>Hwangbo, H.	 
<dd><a href="abstracts/96-215.html"><b>LAUNCH RECOVERY MISSION FOR THE KOREASAT FLIGHT 1</b></a>

<dt>Hwangbo, H. 	 
<dd><a href="abstracts/96-216.html"><b>CONTROL LAW DESIGN FOR AUTONOMOUS STATION COLLOCATION OF SATELLITES</b></a>

<dt>Ih, C-H. C.  	 
<dd><a href="abstracts/96-177.html"><b>ON IMPROVING THE GALILEO SCAN PLATFORM CONE CONTROLLER PERFORMANCE IN CRUISE MODE REMOTE SENSING</b></a>

<dt>Im, S.	 
<dd><a href="abstracts/96-215.html"><b>LAUNCH RECOVERY MISSION FOR THE KOREASAT FLIGHT 1</b></a>

<dt>Irish, K.  	 
<dd><a href="abstracts/96-185.html"><b>PRECISION ORBIT DETERMINATION FOR GFO AND GFO-2</b></a>

<dt>Ishikawa, K. 	 
<dd><a href="abstracts/96-209.html"><b>ON THE INERTIAL MEASUREMENT UNIT USING FIBER OPTIC GYROSCOPES</b></a>

<dt>Jackson, A. A. 	 
<dd><a href="abstracts/96-212.html"><b>A SYMPLETIC MAP FOR GEOSYNCHRONOUS ORBIT PROPAGATION</b></a>

<dt>Jackson, M. 	 
<dd><a href="abstracts/96-131.html"><b>SHUTTLE STABILITY AND CONTROL OF THE STS-71 SHUTTLE/MIR MATED CONFIGURATION</b></a>

<dt>Jackson, M. 	 
<dd><a href="abstracts/96-132.html"><b>IDENTIFICATION OF SHUTTLE/MIR STRUCTURAL DYNAMICS FOR FLIGHT CONTROL NOTCH FILTERING TUNING</b></a>

<dt>Jacobson, R. A. 	 
<dd><a href="abstracts/96-140.html"><b>THE ORBITAL MOTION OF THE MARTIAN SATELLITES: AN APPLICATION OF ARTIFICIAL SATELLITE THEORY</b></a>

<dt>Jalali, M. A. 	 
<dd><a href="abstracts/96-149.html"><b>OPTIMAL GRAVITY-ASSISTED SPACECRAFT TRAJECTORIES FOR OUT-OF-ECLIPTIC INTERPLANETARY MISSIONS</b></a>

<dt>Jang, H. S. 	 
<dd><a href="abstracts/96-109.html"><b>DESIGN OF A DIGITAL LEARNING CONTROLLER USING A PARTIAL ISOMETRY</b></a>

<dt>Jenkins, E. 	 
<dd><a href="abstracts/96-146.html"><b>PARALLEL PROCESSING OF UNCORRELATED OBSERVATIONS INTO SATELLITE ORBITS</b></a>

<dt>Junkins, J. L. 	 
<dd><a href="abstracts/96-172.html"><b>ADAPTIVE EXTERNAL TORQUE ESTIMATION BY MEANS OF TRACKING A LYAPUNOV FUNCTION</b></a>

<dt>Jwo, D. J. 	 
<dd><a href="abstracts/96-210.html"><b>ERROR ANALYSIS AND STABILITY INVESTIGATION OF INTEGRATED GPS/INS NAVIGATION SYSTEMS</b></a>

<dt>Kelm, B. 	 
<dd><a href="abstracts/96-125.html"><b>COMPRESSION OF SATELLITE ORBITS</b></a>

<dt>Kim, S. 	 
<dd><a href="abstracts/96-216.html"><b>CONTROL LAW DESIGN FOR AUTONOMOUS STATION COLLOCATION OF SATELLITES</b></a>

<dt>Kirchwey, K. 	 
<dd><a href="abstracts/96-131.html"><b>SHUTTLE STABILITY AND CONTROL OF THE STS-71 SHUTTLE/MIR MATED CONFIGURATION</b></a>

<dt>Kluever, C. A. 	 
<dd><a href="abstracts/96-100.html"><b>Approximate Solutions for Lunar Trajectory and Vehicle Optimization Using Electric PropULsion</b></a>

<dt>Kluever, C. A. 	 
<dd><a href="abstracts/96-194.html"><b>OPTIMAL LOW THRUST INTERPLANETARY TRAJECTORIES BY DIRECT METHOD TECHNIQUES</b></a>

<dt>Knapp, C. T. 	 
<dd><a href="abstracts/96-103.html"><b>TRAJECTORY DETERMINATION FOR A WEAKLY BOUND TRANSLUNAR TRAJECTORY</b></a>

<dt>Korsmeyer, D. J.	 
<dd><a href="abstracts/96-220.html"><b>EVE, AN INTERACTIVE VIRTUAL OPERATIONS TOOL FOR THE EXTREME ULTRAVIOLET EXPLORER</b></a>

<dt>Kumar, R. R. 	 
<dd><a href="abstracts/96-107.html"><b>AN OPTIMAL CONTROL APPROACH TO NONLINEAR ROBUSTNESS</b></a>

<dt>Kumar, R. R.  	 
<dd><a href="abstracts/96-176.html"><b>ATTITUDE CONTROL AND MOMENTUM MANAGEMENT OF SPACECRAFT BASED ON A SENSITIVITY OBSERVATION</b></a>

<dt>Lanchares, V.  	 
<dd><a href="abstracts/96-139.html"><b>FROZEN ORBITS FOR THE ZONAL MOON POTENTIAL</b></a>

<dt>Lara, M. 	 
<dd><a href="abstracts/96-139.html"><b>FROZEN ORBITS FOR THE ZONAL MOON POTENTIAL</b></a>

<dt>Lee, T. 	 
<dd><a href="abstracts/96-103.html"><b>TRAJECTORY DETERMINATION FOR A WEAKLY BOUND TRANSLUNAR TRAJECTORY</b></a>

<dt>Lee, W.  	 
<dd><a href="abstracts/96-153.html"><b>MISSION PLAN FOR MARS GLOBAL SURVEYOR</b></a>

<dt>Leipold, M. 	 
<dd><a href="abstracts/96-167.html"><b>MAINBELT ASTROID RENDEZVOUS MISSIONS USING SOLAR ELECTRIC AND SOLAR SAIL PROPULSION</b></a>

<dt>Lim, S.  	 
<dd><a href="abstracts/96-205.html"><b>REPEAT GROUND TRACK ANALYSIS FOR THE GEOSCIENCE LASER ALTIMETER SYSTEM</b></a>

<dt>Liquornik, D. J. 	 
<dd><a href="abstracts/96-187.html"><b>MODELING THE INTERNAL EFFECTS WITHIN A HABITABLE MODULE DUE TO A PERFORATION BY AN ORBITAL DEBRIS PARTICLE</b></a>

<dt>Liu, J. J. F.	 
<dd><a href="abstracts/96-137.html"><b>A SET OF REGULAR AND UNIFORM ELEMENTS FOR SATELLITES OF HIGH ECCENTRICITY AND MULTIDAY PERIOD</b></a>

<dt>Longman, R. W. 	 
<dd><a href="abstracts/96-106.html"><b>PHASE CANCELLATION LEARNING CONTROL USING FFT WEIGHTED FREQUENCY RESPONSE IDENTIFICATION</b></a>

<dt>Longman, R. W. 	 
<dd><a href="abstracts/96-109.html"><b>DESIGN OF A DIGITAL LEARNING CONTROLLER USING A PARTIAL ISOMETRY</b></a>

<dt>Longman, R. W. 	 
<dd><a href="abstracts/96-161.html"><b>MONOTONIC VIBRATION SUPPRESSION USING REPETITIVE CONTROL AND WINDOWING TECHNIQUES</b></a>

<dt>Lorenzini, E. C. 	 
<dd><a href="abstracts/96-202.html"><b>STRATEGIES FOR MAXIMIZING THE LIFETIME OF THE SEDSAT SATELLITE</b></a>

<dt>Lorenzini, E. C. 	 
<dd><a href="abstracts/96-201.html"><b>STABILITY OF PENDULAR MOTION OF A TETHER SYSTEM IN AN ELLIPTICAL ORBIT</b></a>

<dt>Mackison, D. L.  	 
<dd><a href="abstracts/96-171.html"><b>ATTDES - AN EXPERT SYSTEM FOR SATELLITE ATTITUDE DETERMINATION AND CONTROL</b></a>

<dt>Maethner, S. R. 	 
<dd><a href="abstracts/96-112.html"><b>DEVELOPMENT OF DOD DEBRIS MITIGATION GUIDELINES</b></a>

<dt>Markin, R. 	 
<dd><a href="abstracts/96-185.html"><b>PRECISION ORBIT DETERMINATION FOR GFO AND GFO-2</b></a>

<dt>Markley, F. L. 	 
<dd><a href="abstracts/96-174.html"><b>PREDICITIVE FILTERING FOR ATTITUDE ESTIMATION WITHOUT RATE SENSORS</b></a>

<dt>Markopoulos, N. 	 
<dd><a href="abstracts/96-200.html"><b>POWER-LIMITED TRANSFERS BETWEEN TWO COPLANAR CONICS UNDER CONTINUOUS KEPLERIAN THRUST</b></a>

<dt>Martinez Benjamin, J. J.  	 
<dd><a href="abstracts/96-204.html"><b>ALTIMETER DATA TREATMENT AND ORBIT SELECTION FOR TOPEX/POSEIDON AND ERS-1</b></a>

<dt>Massmann, F-H. 	 
<dd><a href="abstracts/96-164.html"><b>CROSS-CALIBRATION OF ERS-2 RADAR ALTIMETER USING PRECISION ERS ORBITS</b></a>

<dt>Mazzoleni, A. P.	 
<dd><a href="abstracts/96-219.html"><b>CHAOTIC DYNAMICS IN A SPACECRAFT WITH A FLEXIBLE APPENDAGE AND WITH ENERGY DISSIPATION VIA A NONLINEAR CONTROLLER</b></a>

<dt>McClure, L. H.	 
<dd><a href="abstracts/96-218.html"><b>THE EDUCATIONAL OZONE RESEARCHER:  A 1995 USRA STEDI FINALIST</b></a>

<dt>McFarland, C. A.	 
<dd><a href="abstracts/96-167.html"><b>MAINBELT ASTROID RENDEZVOUS MISSIONS USING SOLAR ELECTRIC AND SOLAR SAIL PROPULSION</b></a>

<dt>McMahon, E. H. 	 
<dd><a href="abstracts/96-177.html"><b>ON IMPROVING THE GALILEO SCAN PLATFORM CONE CONTROLLER PERFORMANCE IN CRUISE MODE REMOTE SENSING</b></a>

<dt>Meehan, P. A.  	 
<dd><a href="abstracts/96-159.html"><b>NONLINEAR INSTABILITIES IN A DUAL-SPIN SPACECRAFT WITH AN AXIAL NUTATIONAL DAMPER</b></a>

<dt>Melvin, P. J. 	 
<dd><a href="abstracts/96-138.html"><b>THE TOPEX ORBIT IN ORLOV'S PLANE AND OTHER APPLICATIONS OF ORBIT LOCAL SPHERICAL HARMONICS</b></a>

<dt>Melvin, P. J. 	 
<dd><a href="abstracts/96-145.html"><b>A KALMAN FILTER FOR ORBIT DETERMINATION WITH APPLICATIONS TO GPS, STELLAR, AND X-RAY NAVIGATION</b></a>

<dt>Merrigan,  M. J. 	 
<dd><a href="abstracts/96-183.html"><b>ORBIT ESTIMATION RESULTS FOR TOPEX/POSEIDON BASED ON GPS TRACKING DATA</b></a>

<dt>Mezhim, V. 	 
<dd><a href="abstracts/96-130.html"><b>STRUCTURAL INTEGRATION OF THE SPACE SHUTTLE AND MIR SPACE STATION</b></a>

<dt>Minter, C. F.  	 
<dd><a href="abstracts/96-156.html"><b>IMPROVEMENTS IN MARS GRAVITY FIELD DETERMINATION USING RIDGE-TYPE ESTIMATION METHODS</b></a>

<dt>Misra, A. 	 
<dd><a href="abstracts/96-175.html"><b>ATTITUDE CONTROL OF SMALL SATELLITES USING FUZZY LOGIC</b></a>

<dt>Mocci, G. 	 
<dd><a href="abstracts/96-213.html"><b>INTER-SATELLITE TRACKING FOR CO-LOCATION</b></a>

<dt>Moe, K. 	 
<dd><a href="abstracts/96-126.html"><b>DRAG COEFFICIENTS OF SPHERES IN FREE-MOLECULAR FLOW</b></a>

<dt>Moe, K. 	 
<dd><a href="abstracts/96-127.html"><b>AN EVALUATION OF JACCHIA 71 AND MSIS90 ATMOSPHERIC MODELS WITH NASA ODERACS DECAY DATA</b></a>

<dt>Moe, M. M.  	 
<dd><a href="abstracts/96-126.html"><b>DRAG COEFFICIENTS OF SPHERES IN FREE-MOLECULAR FLOW</b></a>

<dt>Montenbruck, O. 	 
<dd><a href="abstracts/96-150.html"><b>PERTURBATION FORCES ACTING ON THE ROSETTA SPACECRAFT IN A CLOSE ORBIT AROUND COMET P/WIRTANEN</b></a>

<dt>Morgan, T.	 
<dd><a href="abstracts/96-220.html"><b>EVE, AN INTERACTIVE VIRTUAL OPERATIONS TOOL FOR THE EXTREME ULTRAVIOLET EXPLORER</b></a>

<dt>Mortari, D. 	 
<dd><a href="abstracts/96-158.html"><b>A FAST ON-BOARD AUTONOMOUS ATTITUDE DETERMINATION SYSTEM BASED ON A NEW STAR-ID TECHNIQUE FOR A WIDE FOV STAR TRACKER</b></a>

<dt>Mortari, D. 	 
<dd><a href="abstracts/96-173.html"><b>EULER-q ALGORITHM FOR ATTITUDE DETERMINATION FROM VECTOR OBSERVATIONS</b></a>

<dt>Munk, M. 	 
<dd><a href="abstracts/96-155.html"><b>SPHERE-OF-INFLUENCE TO PLANET-FIXED COORDINATES TARGETING</b></a>

<dt>Munk, M. M. 	 
<dd><a href="abstracts/96-154.html"><b>MISR INTERPLANETARY TRAJECTORY DESIGN</b></a>

<dt>Murata, M.  	 
<dd><a href="abstracts/96-179.html"><b>ORBIT DETERMINATION OF THE ORBITAL RE-ENTRY EXPERIMENT (OREX) SPACECRAFT BY GPS</b></a>

<dt>Nabaa, N. 	 
<dd><a href="abstracts/96-110.html"><b>DERIVATION AND OPTIMALITY OF DISTRIBUTED FILTERING ALGORITHMS BASED ON MINIMUM VARIANCE METHODS</b></a>

<dt>Neal, H. L. 	 
<dd><a href="abstracts/96-146.html"><b>PARALLEL PROCESSING OF UNCORRELATED OBSERVATIONS INTO SATELLITE ORBITS</b></a>

<dt>Newman, J. 	 
<dd><a href="abstracts/96-182.html"><b>FLIGHT TEST RESULTS FROM REAL-TIME RELATIVE GPS FLIGHT EXPERIMENT ON STS-69</b></a>

<dt>O'Connor, B. M. 	 
<dd><a href="abstracts/96-111.html"><b>GENETICALLY PROGRAMMED ADAPTIVE SOFTWARE FOR SPACECRAFT AUTOMATION</b></a>

<dt>Palmerini, G. B. 	 
<dd><a href="abstracts/96-208.html"><b>DESIGN OF SATELLITE CONSTELLATIONS FOR REGIONAL COVERAGE</b></a>

<dt>Pardis, C. J. 	 
<dd><a href="abstracts/96-199.html"><b>SHELLS OF MULTIPLE THRUST IN POWER-LIMITED RENDEZVOUS OF A SPACECRAFT</b></a>

<dt>Park, B. 	 
<dd><a href="abstracts/96-216.html"><b>CONTROL LAW DESIGN FOR AUTONOMOUS STATION COLLOCATION OF SATELLITES</b></a>

<dt>Park, Y. 	 
<dd><a href="abstracts/96-182.html"><b>FLIGHT TEST RESULTS FROM REAL-TIME RELATIVE GPS FLIGHT EXPERIMENT ON STS-69</b></a>

<dt>Pastor, C. L. 	 
<dd><a href="abstracts/96-213.html"><b>INTER-SATELLITE TRACKING FOR CO-LOCATION</b></a>

<dt>Pastrone, D. 	 
<dd><a href="abstracts/96-169.html"><b>INDIRECT APPROACH FOR MINIMUM-FUEL AEROASSISTED TRANSFERS</b></a>

<dt>Patzold, M. 	 
<dd><a href="abstracts/96-150.html"><b>PERTURBATION FORCES ACTING ON THE ROSETTA SPACECRAFT IN A CLOSE ORBIT AROUND COMET P/WIRTANEN</b></a>

<dt>Pelaez, J.  	 
<dd><a href="abstracts/96-202.html"><b>STRATEGIES FOR MAXIMIZING THE LIFETIME OF THE SEDSAT SATELLITE</b></a>

<dt>Pelaez, J.  	 
<dd><a href="abstracts/96-201.html"><b>STABILITY OF PENDULAR MOTION OF A TETHER SYSTEM IN AN ELLIPTICAL ORBIT</b></a>

<dt>Pensa, A. F. 	 
<dd><a href="abstracts/96-118.html"><b>OBSERVATIONS OF DEBRIS IN GEOSYNCHRONOUS ORBITS</b></a>

<dt>Petermann, B. 	 
<dd><a href="abstracts/96-175.html"><b>ATTITUDE CONTROL OF SMALL SATELLITES USING FUZZY LOGIC</b></a>

<dt>Pourtakdoust, S. H. 	 
<dd><a href="abstracts/96-149.html"><b>OPTIMAL GRAVITY-ASSISTED SPACECRAFT TRAJECTORIES FOR OUT-OF-ECLIPTIC INTERPLANETARY MISSIONS</b></a>

<dt>Powell,  G. E. 	 
<dd><a href="abstracts/96-118.html"><b>OBSERVATIONS OF DEBRIS IN GEOSYNCHRONOUS ORBITS</b></a>

<dt>Prussing, J. E. 	 
<dd><a href="abstracts/96-198.html"><b>CLOSED-FORM THRUST ACCELERATION FOR OPTIMAL POWER-LIMITED TRAJECTORIES</b></a>

<dt>Rajasenan, C. 	 
<dd><a href="abstracts/96-164.html"><b>CROSS-CALIBRATION OF ERS-2 RADAR ALTIMETER USING PRECISION ERS ORBITS</b></a>

<dt>Rater, L. M. 	 
<dd><a href="abstracts/96-135.html"><b>SATELLITE MOTION IN A VINTI POTENTIAL</b></a>

<dt>Redd, F. J. 	 
<dd><a href="abstracts/96-193.html"><b>DRACO, A DEMONSTRATION AND RESEARCH GAS CAN ORBITER FOR ADVANCED TECHNOLOGY DEMONSTRATION IN LOW EARTH ORBIT</b></a>

<dt>Reigber, Ch. 	 
<dd><a href="abstracts/96-164.html"><b>CROSS-CALIBRATION OF ERS-2 RADAR ALTIMETER USING PRECISION ERS ORBITS</b></a>

<dt>Reynolds, H. 	 
<dd><a href="abstracts/96-146.html"><b>PARALLEL PROCESSING OF UNCORRELATED OBSERVATIONS INTO SATELLITE ORBITS</b></a>

<dt>Riddle, E. L.	 
<dd><a href="abstracts/96-218.html"><b>THE EDUCATIONAL OZONE RESEARCHER:  A 1995 USRA STEDI FINALIST</b></a>

<dt>Ries, J. C. 	 
<dd><a href="abstracts/96-166.html"><b>A SYSTEMATIC APPROACH TO THE PRECISION ORBIT DETERMINATION OF THE GEOSAT EXACT REPEAT MISSION UTILIZING TRANET DOPPLER DATA</b></a>

<dt>Rim, H. J. 	 
<dd><a href="abstracts/96-165.html"><b>GRAVITY TUNING EXPERIMENTS FOR THE PRECISE ORBIT DETERMINATION OF THE EOS ALTIMETER SATELLITE (EOS ALT/GLAS) USING THE GPS TRACKING DATA</b></a>

<dt>Riuz, M. 	 
<dd><a href="abstracts/96-202.html"><b>STRATEGIES FOR MAXIMIZING THE LIFETIME OF THE SEDSAT SATELLITE</b></a>

<dt>Robinett, R. D. 	 
<dd><a href="abstracts/96-172.html"><b>ADAPTIVE EXTERNAL TORQUE ESTIMATION BY MEANS OF TRACKING A LYAPUNOV FUNCTION</b></a>

<dt>Ruiz, M. 	 
<dd><a href="abstracts/96-201.html"><b>STABILITY OF PENDULAR MOTION OF A TETHER SYSTEM IN AN ELLIPTICAL ORBIT</b></a>

<dt>Sanchez Ariz, D. 	 
<dd><a href="abstracts/96-204.html"><b>ALTIMETER DATA TREATMENT AND ORBIT SELECTION FOR TOPEX/POSEIDON AND ERS-1</b></a>

<dt>Santoni, F. 	 
<dd><a href="abstracts/96-170.html"><b>OPTIMAL DESCENT TRAJECTORIES FOR SCIENTIFIC PAYLOADS USING ICBM-CONVERTED LAUNCHERS</b></a>

<dt>Schaub, H. 	 
<dd><a href="abstracts/96-172.html"><b>ADAPTIVE EXTERNAL TORQUE ESTIMATION BY MEANS OF TRACKING A LYAPUNOV FUNCTION</b></a>

<dt>Schinnerer, R. G. 	 
<dd><a href="abstracts/96-144.html"><b>A GEMINI PUZZLE - OPTICAL IMAGING 30 YEARS AGO</b></a>

<dt>Schonberg, W. P.  	 
<dd><a href="abstracts/96-187.html"><b>MODELING THE INTERNAL EFFECTS WITHIN A HABITABLE MODULE DUE TO A PERFORATION BY AN ORBITAL DEBRIS PARTICLE</b></a>

<dt>Schroeder, C. 	 
<dd><a href="abstracts/96-180.html"><b>STS-69 RELATIVE POSITIONING GPS EXPERIMENT</b></a>

<dt>Schutz,  B. E. 	 
<dd><a href="abstracts/96-165.html"><b>GRAVITY TUNING EXPERIMENTS FOR THE PRECISE ORBIT DETERMINATION OF THE EOS ALTIMETER SATELLITE (EOS ALT/GLAS) USING THE GPS TRACKING DATA</b></a>

<dt>Schutz, B. E.	 
<dd><a href="abstracts/96-180.html"><b>STS-69 RELATIVE POSITIONING GPS EXPERIMENT</b></a>

<dt>Schutz, B. E. 	 
<dd><a href="abstracts/96-186.html"><b>AUTONOMOUS NAVIGATION OF BLOCK II-R GPS SATELLITE USING CROSS-LINK MEASUREMENTS</b></a>

<dt>Schutz, B. E. 	 
<dd><a href="abstracts/96-205.html"><b>REPEAT GROUND TRACK ANALYSIS FOR THE GEOSCIENCE LASER ALTIMETER SYSTEM</b></a>

<dt>Schutz, B. E. 	 
<dd><a href="abstracts/96-206.html"><b>ESTIMATION OF ICE SHEET SURFACE ELEVATION CHANGE FROM THE EOS ALTIMETER SATELLITE (ICESAT) CROSSOVER SIMULATION</b></a>

<dt>Sengoku, A. 	 
<dd><a href="abstracts/96-128.html"><b>MODELING SURFACE FORCES ON THE GEODETIC SATELLITE, AJISAI</b></a>

<dt>Serrano, J. 	 
<dd><a href="abstracts/96-187.html"><b>MODELING THE INTERNAL EFFECTS WITHIN A HABITABLE MODULE DUE TO A PERFORATION BY AN ORBITAL DEBRIS PARTICLE</b></a>

<dt>Settecerri, T. J. 	 
<dd><a href="abstracts/96-127.html"><b>AN EVALUATION OF JACCHIA 71 AND MSIS90 ATMOSPHERIC MODELS WITH NASA ODERACS DECAY DATA</b></a>

<dt>Seybold, C. C. 	 
<dd><a href="abstracts/96-191.html"><b>DEMONSTRATING LUNAR OXYGEN PRODUCTION:  THE TEXAS INTERDISCIPLENARY STUDENT MISSION DESIGN PROJECT</b></a>

<dt>Seywald, H. 	 
<dd><a href="abstracts/96-107.html"><b>AN OPTIMAL CONTROL APPROACH TO NONLINEAR ROBUSTNESS</b></a>

<dt>Seywald, H. 	 
<dd><a href="abstracts/96-176.html"><b>ATTITUDE CONTROL AND MOMENTUM MANAGEMENT OF SPACECRAFT BASED ON A SENSITIVITY OBSERVATION</b></a>

<dt>Sharer, P. 	 
<dd><a href="abstracts/96-104.html"><b>MULTIPLE LUNAR FLYBY TARGETING FOR THE WIND MISSION</b></a>

<dt>Sheppard, R. 	 
<dd><a href="abstracts/96-192.html"><b>THE DATA-CHASER HITCHHIKER PROJECT AS A DEMONSTRATION OF DISTRIBUTED OPERATIONS FOR SMALL PAYLOADS</b></a>

<dt>Shilu, C. 	 
<dd><a href="abstracts/96-157.html"><b>DYNAMIC STABILITY CRITERION OF A SLOW SPIN RE-ENTRY VEHICLE</b></a>

<dt>Shingu, H. 	 
<dd><a href="abstracts/96-209.html"><b>ON THE INERTIAL MEASUREMENT UNIT USING FIBER OPTIC GYROSCOPES</b></a>

<dt>Shrini, T. K. 	 
<dd><a href="abstracts/96-134.html"><b>ANALYTICAL APPROXIMATIONS OF POINT MASS MODEL FOR SUBORBITAL/ORBITAL FLIGHTS</b></a>

<dt>Sidney, W. 	 
<dd><a href="abstracts/96-153.html"><b>MISSION PLAN FOR MARS GLOBAL SURVEYOR</b></a>

<dt>Smith, N. 	 
<dd><a href="abstracts/96-131.html"><b>SHUTTLE STABILITY AND CONTROL OF THE STS-71 SHUTTLE/MIR MATED CONFIGURATION</b></a>

<dt>Soccorsi, F. M.  	 
<dd><a href="abstracts/96-208.html"><b>DESIGN OF SATELLITE CONSTELLATIONS FOR REGIONAL COVERAGE</b></a>

<dt>Sorge, M. E. 	 
<dd><a href="abstracts/96-112.html"><b>DEVELOPMENT OF DOD DEBRIS MITIGATION GUIDELINES</b></a>

<dt>Spehar, P. 	 
<dd><a href="abstracts/96-129.html"><b>SHUTTLE/MIR GNC MISSION OVERVIEW</b></a>

<dt>Spencer, D. B. 	 
<dd><a href="abstracts/96-112.html"><b>DEVELOPMENT OF DOD DEBRIS MITIGATION GUIDELINES</b></a>

<dt>Sridharan, R. 	 
<dd><a href="abstracts/96-117.html"><b>CHARACTERISTICS OF DEBRIS AND IMPLICATIONS FOR DETECTION AND TRACKING</b></a>

<dt>Sridharan, R. 	 
<dd><a href="abstracts/96-214.html"><b>GEOSYNCHRONOUS SURVEILLANCE WITH A SPACE-BASED SENSOR</b></a>

<dt>Sridharan, R.  	 
<dd><a href="abstracts/96-118.html"><b>OBSERVATIONS OF DEBRIS IN GEOSYNCHRONOUS ORBITS</b></a>

<dt>Stokes, H. 	 
<dd><a href="abstracts/96-113.html"><b>INTRODUCING IDES: CHARACTERISING THE ORBITAL DEBRIS ENVIRONMENT IN THE PAST, PRESENT, AND FUTURE</b></a>

<dt>Storch, J. A. 	 
<dd><a href="abstracts/96-133.html"><b>FLUTTER OF SOLAR ARRAYS IN RAREFIED JET PLUMES</b></a>

<dt>Swift, E. R. 	 
<dd><a href="abstracts/96-183.html"><b>ORBIT ESTIMATION RESULTS FOR TOPEX/POSEIDON BASED ON GPS TRACKING DATA</b></a>

<dt>Szebehely, V. 	 
<dd><a href="abstracts/96-137.html"><b>A SET OF REGULAR AND UNIFORM ELEMENTS FOR SATELLITES OF HIGH ECCENTRICITY AND MULTIDAY PERIOD</b></a>

<dt>Tanygin, S. 	 
<dd><a href="abstracts/96-160.html"><b>DYNAMICS OF A NEAR-SYMMETRICAL SPACECRAFT DRIVEN BY A CONSTANT THRUST</b></a>

<dt>Tapley, B. D. 	 
<dd><a href="abstracts/96-186.html"><b>AUTONOMOUS NAVIGATION OF BLOCK II-R GPS SATELLITE USING CROSS-LINK MEASUREMENTS</b></a>

<dt>Taylor, J. V. 	 
<dd><a href="abstracts/96-122.html"><b>LONGITUDINAL ACCELERATION MODELING FOR THE GPS BLOCK IIR SPACECRAFT</b></a>

<dt>Teets, R. B. 	 
<dd><a href="abstracts/96-120.html"><b>AN EXAMINATION OF THE HISTORIES OF INTERESTING DEBRIS SATELLTES</b></a>

<dt>Teofilatto, P.  	 
<dd><a href="abstracts/96-170.html"><b>OPTIMAL DESCENT TRAJECTORIES FOR SCIENTIFIC PAYLOADS USING ICBM-CONVERTED LAUNCHERS</b></a>

<dt>Thorne, J. D.  	 
<dd><a href="abstracts/96-197.html"><b>OPTIMAL CONTINUOUS THRUST ORBIT TRANSFERS</b></a>

<dt>Tsujii,  T. 	 
<dd><a href="abstracts/96-209.html"><b>ON THE INERTIAL MEASUREMENT UNIT USING FIBER OPTIC GYROSCOPES</b></a>

<dt>Tsujii, T. 	 
<dd><a href="abstracts/96-179.html"><b>ORBIT DETERMINATION OF THE ORBITAL RE-ENTRY EXPERIMENT (OREX) SPACECRAFT BY GPS</b></a>

<dt>Tuckness, D. G. 	 
<dd><a href="abstracts/96-196.html"><b>Inclination Change Efficiency: A Geocentric Orbit Transfer Guidance Method Using Continuous Low Thrust</b></a>

<dt>Tuckness, D. G.  	 
<dd><a href="abstracts/96-210.html"><b>ERROR ANALYSIS AND STABILITY INVESTIGATION OF INTEGRATED GPS/INS NAVIGATION SYSTEMS</b></a>

<dt>Vaughan, S. H.  	 
<dd><a href="abstracts/96-122.html"><b>LONGITUDINAL ACCELERATION MODELING FOR THE GPS BLOCK IIR SPACECRAFT</b></a>

<dt>von Braun, C. 	 
<dd><a href="abstracts/96-121.html"><b>CRYOGEN THRUST MODELING FOR MSX EPHEMERIS GENERATION</b></a>

<dt>Wagner, L. A. 	 
<dd><a href="abstracts/96-105.html"><b>CLL LUNAR TRAJECTORY DESIGN</b></a>

<dt>Wagner, L. A. 	 
<dd><a href="abstracts/96-154.html"><b>MISR INTERPLANETARY TRAJECTORY DESIGN</b></a>

<dt>Wahbah, M. M. 	 
<dd><a href="abstracts/96-188.html"><b>PREDICTIVE CONTROLLER FOR SPACE CONTACT SIMULATORS</b></a>

<dt>Walker, R. 	 
<dd><a href="abstracts/96-113.html"><b>INTRODUCING IDES: CHARACTERISING THE ORBITAL DEBRIS ENVIRONMENT IN THE PAST, PRESENT, AND FUTURE</b></a>

<dt>Wallace, S. D. 	 
<dd><a href="abstracts/96-126.html"><b>DRAG COEFFICIENTS OF SPHERES IN FREE-MOLECULAR FLOW</b></a>

<dt>Wallner, R. N. 	 
<dd><a href="abstracts/96-124.html"><b>EARTH GRAVITATIONAL ERROR BUDGET</b></a>

<dt>Wang, Y. P. 	 
<dd><a href="abstracts/96-106.html"><b>PHASE CANCELLATION LEARNING CONTROL USING FFT WEIGHTED FREQUENCY RESPONSE IDENTIFICATION</b></a>

<dt>Wang, Y. P.  	 
<dd><a href="abstracts/96-161.html"><b>MONOTONIC VIBRATION SUPPRESSION USING REPETITIVE CONTROL AND WINDOWING TECHNIQUES</b></a>

<dt>Wilks, N. 	 
<dd><a href="abstracts/96-105.html"><b>CLL LUNAR TRAJECTORY DESIGN</b></a>

<dt>Williams, C. H. 	 
<dd><a href="abstracts/96-151.html"><b>AN ANALYTIC APPROXIMATION TO VERY HIGH SPECIFIC IMPULSE & SPECIFIC POWER INTERPLANETARY SPACE MISSION ANALYSIS</b></a>

<dt>Williams, T. 	 
<dd><a href="abstracts/96-160.html"><b>DYNAMICS OF A NEAR-SYMMETRICAL SPACECRAFT DRIVEN BY A CONSTANT THRUST</b></a>

<dt>Willis, J. 	 
<dd><a href="abstracts/96-192.html"><b>THE DATA-CHASER HITCHHIKER PROJECT AS A DEMONSTRATION OF DISTRIBUTED OPERATIONS FOR SMALL PAYLOADS</b></a>

<dt>Woods-Vedeler, J. A.  	 
<dd><a href="abstracts/96-189.html"><b>ON-ORBIT APPLICATION OF H-INFINITY TO THE MIDDECK ACTIVE CONTROLS EXPERIMENT</b></a>

<dt>Wright, J. R. 	 
<dd><a href="abstracts/96-148.html"><b>RELATIVISTIC ORBIT DETERMINATION</b></a>

<dt>Xing, G. 	 
<dd><a href="abstracts/96-162.html"><b>DEVELOPMENT OF ROBUST REDUCED ORDERED DIGITAL CONTROLLER FOR LARGE ORBITING PLATFORMS IN DISCRETE-TIME DOMAIN</b></a>

<dt>Ying,  N. 	 
<dd><a href="abstracts/96-157.html"><b>DYNAMIC STABILITY CRITERION OF A SLOW SPIN RE-ENTRY VEHICLE</b></a>

<dt>Yoon, S. 	 
<dd><a href="abstracts/96-196.html"><b>Inclination Change Efficiency: A Geocentric Orbit Transfer Guidance Method Using Continuous Low Thrust</b></a>

<dt>Zare, K.  	 
<dd><a href="abstracts/96-137.html"><b>A SET OF REGULAR AND UNIFORM ELEMENTS FOR SATELLITES OF HIGH ECCENTRICITY AND MULTIDAY PERIOD</b></a>

<dt>Zimpfer, D. 	 
<dd><a href="abstracts/96-129.html"><b>SHUTTLE/MIR GNC MISSION OVERVIEW</b></a>

<dt>Zimpfer, D. 	 
<dd><a href="abstracts/96-131.html"><b>SHUTTLE STABILITY AND CONTROL OF THE STS-71 SHUTTLE/MIR MATED CONFIGURATION</b></a>

<dt>Zimpfer, D. 	 
<dd><a href="abstracts/96-.html"><b>Shuttle/Mir Video, etc.</b></a>
</dl>