|
Server : Apache/2.4.62 System : FreeBSD fbsdweb2.web.rcn.net 14.1-RELEASE FreeBSD 14.1-RELEASE releng/14.1-n267679-10e31f0946d8 GENERIC amd64 User : www ( 80) PHP Version : 8.3.8 Disable Function : NONE Directory : /domains/astrosfm/AAS_meetings/1998_winter/ |
Upload File : |
<title>Technical Sessions</title> <Body BGCOLOR = "ffffff"> <h2> 1998 AAS/AIAA Space Flight Mechanics Conference</h2> <h2>Technical Sessions</h2> <dl> <dt><h3>Session 1: Tethered Systems</h3> <h4>Monday, February 9, 8:30 AM / Laguna Ballroom E</h4> <h4>Chair: DR. ARUN K. MISRA, McGill University</h4> <ul> <li><a href="abstracts/98-100.html"><b>AAS 98-100</b></a> -- <b>MISSION ANALYSIS OF A TETHERED SYSTEM FOR LEO TO GEO ORBITAL TRANSFERS, </b>E. C. Lorenzini, M. L. Cosmo - Harvard-Smithsonian Center for Astrophysics; M. Kaiser - Technische Universitat Munchen, Germany; M. Bangham, H. Dionne, D. Vonderwell - The Boeing Co.; L. Johnson - NASA Marshall Space Flight Center <li><a href="abstracts/98-101.html"><b>AAS 98-101</b></a> -- <b>IDENTIFICATION AND ORBIT DETERMINATION OF TETHERED SATELLITE SYSTEM, </b>S. Cho, J. E. Cochran, Jr., D. A. Cicci - Auburn University <li><a href="abstracts/98-102.html"><b>AAS 98-102</b></a> -- <b>ORBIT DETERMINATION OF A TETHERED SATELLITE SYSTEM USING LASER AND RADAR TRACKING, </b>MOVED TO 11:20 <li><a href="abstracts/98-103.html"><b>AAS 98-103</b></a> -- <b>REORIENTATION OF A PLATFORM SUPPORTING A TETHERED SATELLITE SYSTEM, </b>G. Gilardi, V. J. Modi, S. Kalantzis - The University of British Columbia; A. K. Misra - McGill University <li><a href="abstracts/98-104.html"><b>AAS 98-104</b></a> -- <b>ANALYSIS AND DESIGN OF THE AEROBRAKING TETHER FOR STOCHASTIC ERRORS, </b>S. G. Tragesser, J. M. Longuski - Purdue University <li><a href="abstracts/98-105.html"><b>AAS 98-105</b></a> -- <b>ON THE DEPLOYMENT OF AN ELECTRODYNAMIC TETHER FROM AN ELLIPTICAL ORBIT, </b>M. Ruiz, J. Pelaez - Universidad Politecnica de Madrid, Spain </ul> <dt><h3>Session 2: Interplanetary Missions 1</h3> <h4>Monday, February 9, 8:30 AM / Laguna Ballroom F</h4> <h4>Chair: DR. LINCOLN J. WOOD, Jet Propulsion Laboratory</h4> <ul> <li><a href="abstracts/98-106.html"><b>AAS 98-106</b></a> -- <b>DESCRIPTION OF THREE CANDIDATE CASSINI SATELLITE TOURS, </b>J. C. Smith - Jet Propulsion Laboratory <li><a href="abstracts/98-107.html"><b>AAS 98-107</b></a> -- <b>INCORPORATING ICY SATELLITE FLYBYS IN THE CASSINI ORBITAL TOUR, </b>A. A. Wolf - Jet Propulsion Laboratory <li><a href="abstracts/98-108.html"><b>AAS 98-108</b></a> -- <b>NAVIGATION FEASIBILITY STUDIES FOR THE EUROPA ORBITER MISSION, </b>M. D. Guman, D. C. Roth, B. G. Williams - Jet Propulsion Laboratory <li><a href="abstracts/98-109.html"><b>AAS 98-109</b></a> -- <b>WITHDRAWN </b> <li><a href="abstracts/98-110.html"><b>AAS 98-110</b></a> -- <b>MARS AEROCAPTURE STUDIES FOR THE DESIGN REFERENCE MISSION, </b>J. E. Lyne - University of Tennessee; P. Wercinski - NASA Ames Research Center; G. Walberg, R. Jits - North Carolina State University <li><a href="abstracts/98-111.html"><b>AAS 98-111</b></a> -- <b>NON-TYPICAL TRAJECTORY ALTERNATIVES FOR MARS CARGO MISSIONS, </b>B. M. Portock - University of Tennessee Space Institute; J. E. Lyne - University of Tennessee; G. A. Flandro - University of Tennessee Space Institute <li><a href="abstracts/98-112.html"><b>AAS 98-112</b></a> -- <b>MARS GLOBAL SURVEYOR AEROBRAKING AT MARS, </b>M. D. Johnson, P. B. Esposito, V. Alwar - Jet Propulsion Laboratory; S. W. Demcak - OAO Corporation; E. J. Graat, R. A. Mase - JPL </ul> <dt><h3>Session 3: Tracking and Navigation</h3> <h4>Monday, February 9, 8:30 AM / Laguna Ballroom G</h4> <h4>Chair: DR. CATHERINE L. THORNTON, Jet Propulsion Laboratory</h4> <ul> <li><a href="abstracts/98-113.html"><b>AAS 98-113</b></a> -- <b>DEMONSTRATION OF A SPECIAL-PERTURBATIONS-BASED CATALOG IN THE NAVAL SPACE COMMAND SYSTEM, </b>S. L. Coffey - Naval Research Laboratory; H. L. Neal - GRC International; C. L. Visel- HQ USSPACECOM; P. Conolly - Naval Space Command <li><a href="abstracts/98-114.html"><b>AAS 98-114</b></a> -- <b>OBJECT ORIENTED EPHEMERIS GENERATION IN A DISTRIBUTED COMPUTING ENVIRONMENT WITH JAVA, </b>J. G. Kasalo - Santa Clara, CA <li><a href="abstracts/98-115.html"><b>AAS 98-115</b></a> -- <b>SINGLE TRACK COVARIANCE FOR SPACE SURVEILLANCE NETWORK SENSORS, </b>K. T. Alfriend - Texas A&M University; F. Hoots, R. A. Glover, R. G. France - GRC International <li><a href="abstracts/98-116.html"><b>AAS 98-116</b></a> -- <b>DESIGN FOR OPERATIONAL CALIBRATION OF THE NAVAL SPACE SURVEILLANCE SYSTEM, </b>P. W. Schumacher, Jr. - Naval Space Command; G. C. Gilbreath - Naval Research Laboratory; E. D. Lydick, S. G. Walters - Naval Space Command; M. A. Davis, J. H. Seago - Allied Signal Technical Services Corp. <li><a href="abstracts/98-117.html"><b>AAS 98-117</b></a> -- <b>ESTIMATION OF RADAR ORIENTATION, LOCATION AND OTHER CALIBRATION PARAMETERS USING REGULARIZED RESIDUALS, </b>M. F. Storz - Falcon AFB Space Warfare Center <li><a href="abstracts/98-118.html"><b>AAS 98-118</b></a> -- <b>ANALYSIS OF THE TELSTAR-401/GOES-10 CLOSE APPROACH USING THE RAVEN TELESCOPE, </b>C. Sabol - University of Colorado; R. Burns, S. Wallace - Kirkland AFB </ul> <dt><h3>Session 4: Control Theory and Applications</h3> <h4>Monday, February 9, 1:30 PM / Laguna Ballroom E</h4> <h4>Chair: DR. THOMAS E. CARTER, Eastern Connecticut State University</h4> <ul> <li><a href="abstracts/98-119.html"><b>AAS 98-119</b></a> -- <b>BRIDGING LEARNING CONTROL AND REPETITIVE CONTROL USING BASIS FUNCTIONS, </b>Hao-Ping Wen - Columbia Universtiy; M. Q. Phan - Princeton Universtiy; R. W. Longman - Columbia University <li><a href="abstracts/98-120.html"><b>AAS 98-120</b></a> -- <b>IMPLEMENTING TIME OPTIMAL ROBOT MANEUVERS USING REALISTIC ACTUATOR CONSTRAINTS AND LEARNING CONTROL, </b>Ju Li, R. W. Longman - Columbia University; V. H. Schulz - University of Stuttgart, Germany; H. G. Bock - University of Heidelberg, Germany <li><a href="abstracts/98-121.html"><b>AAS 98-121</b></a> -- <b>STRUCTURED MODEL REFERENCE ADAPTIVE CONTROL IN THE PRESENCE OF BOUNDED DISTURBANCES, </b>M. R. Akella, J. L. Junkins - Texas A&M University <li><a href="abstracts/98-122.html"><b>AAS 98-122</b></a> -- <b>WITHDRAWN </b> <li><a href="abstracts/98-123.html"><b>AAS 98-123</b></a> -- <b>INTEGRATION OF COMET CENTROIDING, ATTITUDE DISTURBANCE REJECTION AND STEERING MIRROR CONTROL FOR THE STARDUST MISSION, </b>L. A. Sachi, P. G. Good - Lockheed Martin Astronautics; S. Bhaskaran - Jet Propulsion Laboratory <li><a href="abstracts/98-124.html"><b>AAS 98-124</b></a> -- <b>THE HIGH ACCURACY DIGITAL SERVO CONTROL AND DATA PROCESSING SYSTEM OF THE ANTENNA PLATFORM IN THE SATELLITE ORBIT SIMULATION LABORATORY, </b>Yan, Jie - Northwestern Polytechnical University, P. R. China </ul> <dt><h3>Session 5: Orbital Dynamics</h3> <h4>Monday, February 9, 1:30 PM / Laguna Ballroom F</h4> <h4>Chair: DR. SHANNON L. COFFEY, Naval Research Laboratory</h4> <ul> <li><a href="abstracts/98-125.html"><b>AAS 98-125</b></a> -- <b>WITHDRAWN </b> <li><a href="abstracts/98-126.html"><b>AAS 98-126</b></a> -- <b>HARMONIC OSCILLATOR SOLUTIONS TO LINEARIZABLE PERTURBATIONS OF TWO-BODY PROBLEMS, </b>I. Aparicio, L. Floria - Universidad de Valladolid, Spain <li><a href="abstracts/98-127.html"><b>AAS 98-127</b></a> -- <b>AN ANALYTICAL THEORY FOR TESSERAL HARMONIC PERTURBATIONS, </b>A. M. Segerman - GRC International; S. L. Coffey - Naval Research Laboratory <li><a href="abstracts/98-128.html"><b>AAS 98-128</b></a> -- <b>SATELLITE CONSTELLATION DESIGN FOR ZONAL COVERAGE USING GENETIC ALGORITHMS, </b>T. A. Ely, W. A. Crossley, E. A. Williams - Purdue University <li><a href="abstracts/98-129.html"><b>AAS 98-129</b></a> -- <b>AN ALGORITHM FOR SIMULATION OF MOTIONS OF 'VARIABLE MASS' SYSTEMS, </b>S. Djerassi - Haifa, Israel <li><a href="abstracts/98-130.html"><b>AAS 98-130</b></a> -- <b>SEARCHING FOR REPEATING GROUND TRACK ORBITS: A SYSTEMATIC APPROACH, </b>M. Lara - Real Instituto y Observatorio de la Armada, Spain <li><a href="abstracts/98-131.html"><b>AAS 98-131</b></a> -- <b>NON-INTEGRABILITY AND CHAOS IN SATELLITE ORBITAL DYNAMICS, </b>M. E. Sansaturio - E.T.S de Ingenieros Industriales, Spain; I. Vigo-Aguiar, J. M. Ferrandiz - Universidat de Alicante, Spain </ul> <dt><h3>Session 6: Mission Analysis</h3> <h4>Monday, February 9, 1:30 PM / Laguna Ballroom G</h4> <h4>Chair: DR. C. DAVID EAKMAN, Boeing Company</h4> <ul> <li><a href="abstracts/98-132.html"><b>AAS 98-132</b></a> -- <b>EXACT ANALYTICAL SOLUTION TO A THREE-DIMENSIONAL INTERCEPTION OF A MANEUVERING TARGET, </b>N. X. Vinh, P. T. Kabamba, T. Takehira - The University of Michigan <li><a href="abstracts/98-133.html"><b>AAS 98-133</b></a> -- <b>WITHDRAWN </b> <li><a href="abstracts/98-134.html"><b>AAS 98-134</b></a> -- <b>DETERMINATION OF CLOSE APPROACHES FOR EARTH-FIXED LAUNCH TRAJECTORIES, </b>J. Woodburn - Analytical Graphics, Inc. <li><a href="abstracts/98-135.html"><b>AAS 98-135</b></a> -- <b>HUMAN MARS EXPLORATION: STUDENT-DESIGNED MISSIONS AND THE CURRENT NASA REFERENCE MISSION, </b>C. C. Seybold, W.T. Fowler - The University of Texas at Austin <li><a href="abstracts/98-136.html"><b>AAS 98-136</b></a> -- <b>LOW ENERGY INTERPLANETARY TRANSFERS USING THE INVARIANT MANIFOLDS OF L1, L2, AND HALO ORBITS, </b>M. W. Lo, S. D. Ross - Jet Propulsion Laboratory <li><a href="abstracts/98-137.html"><b>AAS 98-137</b></a> -- <b>WITHDRAWN </b> <li><a href="abstracts/98-138.html"><b>AAS 98-138</b></a> -- <b>CHALLENGES POSED BY HYPER-LIGHT TRAJECTORIES, </b>P. A. Murad - Vienna, VA </ul> <dt><h3>Session 7: Attitude Control</h3> <h4>Tuesday, February 10, 8:30 AM / Laguna Ballroom E</h4> <h4>Chair: MR. ALFRED J. TREDER, Boeing Defense and Space Group</h4> <ul> <li><a href="abstracts/98-139.html"><b>AAS 98-139</b></a> -- <b>ATTITUDE CONTROL ISSUES ASSOCIATED WITH FLEXIBLE AND LOOSELY CONNECTED APPENDAGES, </b>S. Tanygin, T. Williams - University of Cincinnati <li><a href="abstracts/98-140.html"><b>AAS 98-140</b></a> -- <b>FEEDBACK CONTROL LAW FOR VARIABLE SPEED CONTROL MOMENT GYROS, </b>H. Schaub, S. R. Vadali, J. L. Junkins - Texas A&M University <li><a href="abstracts/98-141.html"><b>AAS 98-141</b></a> -- <b>OPTIMAL DESIGN OF A PASSIVE CONING ATTENUATOR FOR SPINNING SPACECRAFT UNDER THRUST, </b>D. M. Halsmer, A. R. Fetter - Oral Roberts University <li><a href="abstracts/98-142.html"><b>AAS 98-142</b></a> -- <b>STARDUST TCM AND DESPIN IN THE PRESENCE OF COMPLEX FUEL DYNAMICS, </b>P. Good, A. Carpenter, H. Flanders, T. Gardner - Lockheed Martin Astronautics <li><a href="abstracts/98-143.html"><b>AAS 98-143</b></a> -- <b>AN ANALYSIS OF SHUTTLE-BASED PERFORMANCE OF MEMS SENSORS, </b>R. H. Smith - The Aerospace Corp. <li><a href="abstracts/98-144.html"><b>AAS 98-144</b></a> -- <b>WITHDRAWN </b>I </ul> <dt><h3>Session 8: Interplanetary Missions 2</h3> <h4>Tuesday, February 10, 8:30 AM / Laguna Ballroom F</h4> <h4>Chair: DR. RICHARD HOLDAWAY, Rutherford Appleton Laboratory</h4> <ul> <li><a href="abstracts/98-145.html"><b>AAS 98-145</b></a> -- <b>NAVIGATION FLIGHT OPERATIONS FOR MARS PATHFINDER, </b>R. M. Vaughan, P. H. Kallemeyn, D. A. Spencer - Jet Propulsion Laboratory; R. D. Braun - NASA Langley Research Center <li><a href="abstracts/98-146.html"><b>AAS 98-146</b></a> -- <b>MARS PATHFINDER ATMOSPHERIC ENTRY RECONSTRUCTION, </b>D. A. Spencer - Jet Propulsion Laboratory; R. C. Blanchard - NASA Langley Research Center; S. W. Thurman - JPL; R. D. Braun - NASA LaRC; C.-Y. Peng, P. H. Kallemeyn - JPL </ul> <dt><h3>Chair: DR. RICHARD HOLDAWAY</h3> <h4>8:30 AM / Laguna Ballroom F, Session 8: Interplanetary Missions 2</h4> <h4>, Rutherford Appleton Laboratory</h4> <ul> <li><a href="abstracts/98-147.html"><b>AAS 98-147</b></a> -- <b>ENTRY TRAJECTORY DISPERSIONS DUE TO UNCERTAINTIES IN THE MARS ATMOSPHERE, </b>G. E. Peterson - The Aerospace Corp.; R. H. Bishop - University of Texas at Austin </ul> <dt><h3>Session 8: Interplanetary Missions 2</h3> <h4>Tuesday, February 10, 8:30 AM / Laguna Ballroom F</h4> <h4>Chair: DR. RICHARD HOLDAWAY, Rutherford Appleton Laboratory</h4> <ul> <li><a href="abstracts/98-148.html"><b>AAS 98-148</b></a> -- <b>MINIMUM-FUEL ESCAPE FROM TWO-BODY EARTH-SUN SYSTEM, </b>L. Casalino, G. Colasurdo - Politecnico di Torino, Italy; E. Fantino - Universita di Padova, Italy <li><a href="abstracts/98-149.html"><b>AAS 98-149</b></a> -- <b>LAUNCH PERIOD ANALYSIS FOR THE JUPITER GRAVITY ASSIST OPPORTUNITIES TO PLUTO, </b>M. D. Reyes - Naval Postgraduate School; S. E. Matousek - Jet Propulsion Laboratory; I. M. Ross - Naval Postgraduate School <li><a href="abstracts/98-150.html"><b>AAS 98-150</b></a> -- <b>WITHDRAWN </b> </ul> <dt><h3>Session 9: Reference Systems and Simulation</h3> <h4>Tuesday, February 10, 8:30 AM / Laguna Ballroom G</h4> <h4>Chair: DR. BRUCE J. HAINES, Jet Propulsion Laboratory</h4> <ul> <li><a href="abstracts/98-151.html"><b>AAS 98-151</b></a> -- <b>THE INTERNATIONAL CELESTIAL REFERENCE SYSTEM, </b>P. K. Seidelmann - U.S. Naval Observatory <li><a href="abstracts/98-152.html"><b>AAS 98-152</b></a> -- <b>THE NEW STAR CATALOGS, </b>P. K. Seidelmann, T. Corbin - U.S. Naval Observatory <li><a href="abstracts/98-153.html"><b>AAS 98-153</b></a> -- <b>THE 488,006,860 STARS IN THE USNO-A1.0 CATALOG, </b>D. G. Monet - U.S. Naval Observatory Flagstaff Station <li><a href="abstracts/98-154.html"><b>AAS 98-154</b></a> -- <b>FIZEAU ASTROMETRIC MAPPING EXPLORER (FAME) SATELLITE, </b>P. K. Seidelmann - U.S. Naval Observatory <li><a href="abstracts/98-155.html"><b>AAS 98-155</b></a> -- <b>AN ANALYSIS OF THE BEHAVIOR OF THE J2000 REDUCTION MATRICES, </b>D. A. Vallado - Phillips Laboratory </ul> <dt><h3>Session 10: Estimation</h3> <h4>Tuesday, February 10, 1:30 PM / Laguna Ballroom E</h4> <h4>Chair: DR. CHRISTOPHER D. HALL, Virginia Polytechnic Institute and State University</h4> <ul> <li><a href="abstracts/98-156.html"><b>AAS 98-156</b></a> -- <b>TOPEX/POSEIDON "QUICK-LOOK" PRECISION ORBIT DETERMINATION IMPROVEMENT AND PERFORMANCE, </b>A. H. Salama, B. M. Kennedy - Jet Propulsion Laboratory <li><a href="abstracts/98-157.html"><b>AAS 98-157</b></a> -- <b>NONLINEAR ADAPTIVE STATE ESTIMATOR APPROACH TO ATTITUDE AND ORBIT DETERMINATION USING ONLY A MAGNETOMETER, </b>F. Curti - University of Rome "La Sapienza", Italy <li><a href="abstracts/98-158.html"><b>AAS 98-158</b></a> -- <b>WAVELETS, SMOOTHERS, AND FILTERS - APPLICATION TO SATELLITE ATTITUDE DETERMINATION PROBLEMS, </b>D. L. Mackison - University of Colorado <li><a href="abstracts/98-159.html"><b>AAS 98-159</b></a> -- <b>TOWARD THE MOST ACCURATE ATTITUDE DETERMINATION SYSTEM USING STAR TRACKERS, </b>D. Mortari - Universita degli Studi "La Sapienza" di Roma, Italy; T. C. Pollock, J. L. Junkins - Texas A&M University <li><a href="abstracts/98-160.html"><b>AAS 98-160</b></a> -- <b>WITHDRAWN </b> <li><a href="abstracts/98-161.html"><b>AAS 98-161</b></a> -- <b>APPLICATION OF AVERAGE CONTAMINATION SOURCES FOR THE PREDICTION OF SPACE DEBRIS ENVIRONMENT, </b>A. I. Nazarenko - Center for Program Studies, Russia </ul> <dt><h3>Session 11: Optimization Theory and Applications</h3> <h4>Tuesday, February 10, 1:30 PM / Laguna Ballroom F</h4> <h4>Chair: DR. CRAIG A. KLUEVER, University of Missouri - Columbia/Kansas City</h4> <ul> <li><a href="abstracts/98-162.html"><b>AAS 98-162</b></a> -- <b>WITHDRAWN </b> <li><a href="abstracts/98-163.html"><b>AAS 98-163</b></a> -- <b>NECESSARY AND SUFFICIENT CONDITIONS FOR OPTIMAL CONTROL PROBLEMS WITH SCALAR TERMINAL CONSTRAINT, </b>Jang-Won Jo, J. E. Prussing - University of Illinois at Urbana-Champaign <li><a href="abstracts/98-164.html"><b>AAS 98-164</b></a> -- <b>NECESSARY AND SUFFICIENT CONDITIONS FOR OPTIMAL CONTROL PROBLEMS WITH MULTIPLE TERMINAL CONSTRAINTS, </b>Jang-Won Jo, J. E. Prussing - University of Illinois at Urbana-Champaign <li><a href="abstracts/98-165.html"><b>AAS 98-165</b></a> -- <b>OPTIMIZATION OF SOLAR-PERTURBED DOUBLE LUNAR SWINGBY ESCAPE TRAJECTORIES, </b>C. R. Cassell - University of California, San Diego <li><a href="abstracts/98-166.html"><b>AAS 98-166</b></a> -- <b>APPLICATION OF OPTIMAL PERIODIC CONTROL THEORY TO THE ORBIT REBOOST PROBLEM, </b>K. E. Jensen, F. Fahroo, I. M. Ross - Naval Postgraduate School <li><a href="abstracts/98-167.html"><b>AAS 98-167</b></a> -- <b>WITHDRAWN </b> </ul> <dt><h3>Session 12: Near Earth Mission Design</h3> <h4>Tuesday, February 10, 1:30 PM / Laguna Ballroom G</h4> <h4>Chair: DR. DAVID B. SPENCER, USAF Phillips Laboratory</h4> <ul> <li><a href="abstracts/98-168.html"><b>AAS 98-168</b></a> -- <b>STATION-KEEPING STRATEGIES FOR TRANSLUNAR LIBRATION POINT ORBITS, </b>G. Gomez - Universitat de Barcelona, Spain; K. C. Howell - Purdue University; J. Masdemont - Universitat Politecnica de Catalunya, Spain; C. Simo - Universitat de Barcelona, Spain <li><a href="abstracts/98-169.html"><b>AAS 98-169</b></a> -- <b>FORMATION FLYING IN THE VICINITY OF LIBRATION POINT ORBITS, </b>B. T. Barden, K. C. Howell - Purdue University <li><a href="abstracts/98-170.html"><b>AAS 98-170</b></a> -- <b>ECLIPSES BY THE EARTH AND BY THE MOON AS CONSTRAINTS ON THE AXAF MISSION, </b>S. W. Evans - Marshall Space Flight Center <li><a href="abstracts/98-171.html"><b>AAS 98-171</b></a> -- <b>ON-ORBIT ENGINEERING TESTS OF AERCAM SPRINT ROBOTIC CAMERA VEHICLE, </b>T. Williams, S. Tanygin - University of Cincinnati <li><a href="abstracts/98-172.html"><b>AAS 98-172</b></a> -- <b>CONTINUOUS GLOBAL EARTH COVERAGE BY MEANS OF MULTISTATIONARY ORBITS, </b>M. M. Castronuovo, A. Bardone, M. Di Ruscio - Universita degli Studi di Roma "La Sapienza", Italy <li><a href="abstracts/98-173.html"><b>AAS 98-173</b></a> -- <b>THE 1997.0 CNUCE ORBITAL DEBRIS REFERENCE MODEL, </b>C. Pardini, L. Anselmo, A. Rossi - CNUCE/CNR, Italy; A. Cordelli - Consorzio Pisa Ricerche, Italy; P. Farinella - Universitai di Pisa, Italy <li><a href="abstracts/98-174.html"><b>AAS 98-174</b></a> -- <b>THE REALITIES OF REENTRY DISPOSAL, </b>R. P. Patera, W. H. Ailor - The Aerospace Corp. </ul> <dt><h3>Session 13: Space Structures</h3> <h4>Wednesday, February 11, 8:30 AM / Laguna Ballroom E</h4> <h4>Chair: DR. PETER M. BAINUM, Howard University</h4> <ul> <li><a href="abstracts/98-175.html"><b>AAS 98-175</b></a> -- <b>EFFECT OF NONLINEARITY ON THE DYNAMICS OF SPINNING SPACECRAFT APPENDAGES WITH AN OFFSET, </b>A. K. Misra, M. J. Sadigh - McGill University; G. Tyc - Bristol Aerospace Ltd.; V. J. Modi - University of British Columbia <li><a href="abstracts/98-176.html"><b>AAS 98-176</b></a> -- <b>WITHDRAWN </b> <li><a href="abstracts/98-177.html"><b>AAS 98-177</b></a> -- <b>DEPLOYABLE ANTENNA TEST FACILITY WITH MAGNETICALLY SUSPENDED SLIDERS (MAGSUS SLIDERS), </b>Y. Horiuchi, T. Sugimoto - Mitsubishi Electric Corp., Japan; H. Tsunoda, Y. Kawakami - Advanced Space Communication Research Laboratory, Japan <li><a href="abstracts/98-178.html"><b>AAS 98-178</b></a> -- <b>WITHDRAWN </b> <li><a href="abstracts/98-179.html"><b>AAS 98-179</b></a> -- <b>STUDY OF SENSOR REDUNDANCY AND EFFECT OF ACCELEROMETER FOR FLEXIBLE EXPENDABLE LAUNCH VEHICLES (ELV), </b>Zhaozhi Tan, P. M. Bainum - Howard University <li><a href="abstracts/ 98-18.html"><b>AAS 98-18</b></a> -- <b>WITHDRAWN </b> <li><a href="abstracts/98-181.html"><b>AAS 98-181</b></a> -- <b>STABILITY AND COUPLING CHARACTERISTICS OF FLIGHT VEHICLE CONSIDER WITH ELASTIC FREEDOM, </b>Tang, Shuo; Li, Xiaolong - Northwestern Polytechnical University, P. R. China </ul> <dt><h3>Session 14: Comet and Asteroid Missions</h3> <h4>Wednesday, February 11, 8:30 AM / Laguna Ballroom F</h4> <h4>Chair: DR. I. MICHAEL ROSS, Naval Postgraduate School</h4> <ul> <li><a href="abstracts/98-182.html"><b>AAS 98-182</b></a> -- <b>PLANNING A FASTER, CHEAPER ASTEROID MISSION, </b>A. S. Hope - Naval Research Laboratory <li><a href="abstracts/98-183.html"><b>AAS 98-183</b></a> -- <b>ASTEROID SELECTION AND MISSION DESIGN FOR SPACEDEVCO'S NEAR-EARTH ASTEROID PROSPECTOR, </b>C. R. Cassell - UCSD and Lockheed-Martin Missiles and Space Corp.; A. M. Schneider, R. Gulman, R. Lee, E. Estey - University of California at San Diego <li><a href="abstracts/98-184.html"><b>AAS 98-184</b></a> -- <b>MISSION DESIGN AND NAVIGATION OF NEAR'S ENCOUNTER WITH ASTEROID 253 MATHILDE, </b>D. J. Scheeres - Iowa State University; D. W. Dunham, R. W. Farquhar - Applied Physics Laboratory; C. E. Helfrich - Jet Propulsion Laboratory; J. V. McAdams - APL; W. M. Owen, Jr., S. P. Synnott, B. G. Williams, P. J. Wolff, D. K. Yeomans - JPL <li><a href="abstracts/98-185.html"><b>AAS 98-185</b></a> -- <b>AUTONOMOUS CONTROLLED LANDING ON COMETARY BODIES, </b>S. Dawson, C. W. Potterveld, H. Konigsmann, L. Early - Microcosm Inc. <li><a href="abstracts/98-186.html"><b>AAS 98-186</b></a> -- <b>GRAVITATIONAL EFFECTS OF EARTH IN OPTIMIZING DELTA-V FOR DEFLECTING EARTH-CROSSING ASTEROIDS, </b>Sang-Young Park, I. M. Ross - Naval Postgraduate School <li><a href="abstracts/98-187.html"><b>AAS 98-187</b></a> -- <b>MISSION DESIGN FOR THE DEEP SPACE 4/CHAMPOLLION COMET SAMPLE RETURN MISSION, </b>G. H. Tan-Wang, J. A. Sims - Jet Propulsion Laboratory </ul> <dt><h3>Session 15: Orbit Determination</h3> <h4>Wednesday, February 11, 8:30 AM / Laguna Ballroom G</h4> <h4>Chair: DR. PAUL J. CEFOLA, The Charles Stark Draper Laboratory</h4> <ul> <li><a href="abstracts/98-188.html"><b>AAS 98-188</b></a> -- <b>WITHDRAWN </b> <li><a href="abstracts/98-189.html"><b>AAS 98-189</b></a> -- <b>MODELING CATASTROPHIC DECAY ORBITS THROUGH PERIGEE, </b>J. D. Fischer - USAF, Massachusetts Institute of Technology; P. J. Cefola, R. J. Proulx - C. S. Draper Laboratory <li><a href="abstracts/98-190.html"><b>AAS 98-190</b></a> -- <b>ESTIMATING ATMOSPHERE DENSITY VARIATIONS TO IMPROVE LEO ORBIT PREDICTION ACCURACY, </b>A. I. Nazarenko - Center for Program Studies, Russia; P. J. Cefola - C. S. Draper Laboratory; V. Yurasov - Space Research Center Kosmos, Russia <li><a href="abstracts/98-191.html"><b>AAS 98-191</b></a> -- <b>DETERMINATION AND PREDICTION OF ORBITS WITH DUE ACCOUNT OF DISTURBANCES AS A "COLOR" NOISE, </b>A. I. Nazarenko - Center for Program Studies, Russia <li><a href="abstracts/98-192.html"><b>AAS 98-192</b></a> -- <b>SIMULTANEOUS ORBIT DETERMINATION OF LARGE SATELLITE CONSTELLATIONS, </b>M. T. Soyka, J. W. Middour - Naval Research Laboratory; J. Fein - Computer Sciences Corp. <li><a href="abstracts/98-193.html"><b>AAS 98-193</b></a> -- <b>ORBIT DETERMINATION PERFORMANCE EVALUATION OF THE DEEP SPACE 1 AUTONOMOUS NAVIGATION SYSTEM, </b>S. Bhaskaran, S. D. Desai, P. J. Dumont, B. M. Kennedy, G. W. Null, W. M. Owen, J. E. Riedel, S. P. Synnott, R. A. Werner - Jet Propulsion Laboratory </ul> <dt><h3>Session 16: GPS Applications</h3> <h4>Wednesday, February 11, 1:30 PM / Laguna Ballroom E</h4> <h4>Chair: DR. BOBBY G. WILLIAMS, Jet Propulsion Laboratory</h4> <ul> <li><a href="abstracts/98-194.html"><b>AAS 98-194</b></a> -- <b>RESULTS OF STS-80 RELATIVE GPS NAVIGATION FLIGHT EXPERIMENT, </b>E. R. Schiesser, J. P. Brazzel, Jr. - The Boeing Company; J. R. Carpenter, H. D. Hinkel - NASA Johnson Space Center <li><a href="abstracts/98-195.html"><b>AAS 98-195</b></a> -- <b>LEO ORBIT DETERMINATION WITH DIFFERENTIAL GPS, </b>P. J. Melvin - Naval Research Laboratory <li><a href="abstracts/98-196.html"><b>AAS 98-196</b></a> -- <b>SATELLITE TO SATELLITE RELATIVE NAVIGATION USING GPS SIGNAL SIMULATORS, </b>P. W. Binning - Naval Research Laboratory <li><a href="abstracts/98-197.html"><b>AAS 98-197</b></a> -- <b>PRECISE ORBIT DETERMINATION FOR THE MOMS/PRIRODA CAMERA EXPERIMENT BASED ON DGPS CARRIER-PHASE AND PSEUDO-RANGE MEASUREMENTS, </b>D. C. Kuijper - German Space Operations Center (GSOC), Germany <li><a href="abstracts/98-198.html"><b>AAS 98-198</b></a> -- <b>CONTROL OF SPACE STATION AND ITS ADJOINT ORBITER USING RELATIVE DGPS, </b>Jianping Yuan, Jianjun Luo, Xiaomu Dou, Zhongyuan Tian - Northwestern Polytechnical University, P. R. China <li><a href="abstracts/98-199.html"><b>AAS 98-199</b></a> -- <b>GPS ATTITUDE DETERMINATION BY KALMAN FILTERING: SIMULATION OF MULTIPATH REJECTION, </b>F. Bernelli-Zazzera - Politecnico di Milano, Italy; R. Campana, F. Gottifredi, L. Marradi - LABEN S.p.A., Italy </ul> <dt><h3>Session 17: Low Thrust Missions and Analysis</h3> <h4>Wednesday, February 11, 1:30 PM / Laguna Ballroom F</h4> <h4>Chair: DR. ROBERT G. MELTON, Pennsylvania State University</h4> <ul> <li><a href="abstracts/98-200.html"><b>AAS 98-200</b></a> -- <b>OPTIMAL LOW-THRUST TRAJECTORIES USING FLYBY, </b>L. Casalino, G. Colasurdo, D. Pastrone - Politecnico di Torino, Italy <li><a href="abstracts/98-201.html"><b>AAS 98-201</b></a> -- <b>NAVIGATION CONSIDERATIONS FOR LOW-THRUST PLANETARY MISSIONS, </b>P. J. Wolff, F. Pinto, B. G. Williams, R. M. Vaughan - Jet Propulsion Laboratory <li><a href="abstracts/98-202.html"><b>AAS 98-202</b></a> -- <b>OPTIMAL INTERPLANETARY SPACECRAFT TRAJECTORIES VIA A PARETO GENETIC ALGORITHM, </b>J. W. Hartmann, V. L. Coverstone-Carroll - University of Illinois at Urbana-Champaign; S. N. Williams - Jet Propulsion Laboratory <li><a href="abstracts/98-203.html"><b>AAS 98-203</b></a> -- <b>SIMPLE CONTROL LAWS FOR LOW-THRUST ORBIT TRANSFERS, </b>C. A. Kluever - University of Missouri-Columbia/Kansas City <li><a href="abstracts/98-204.html"><b>AAS 98-204</b></a> -- <b>FLYWHEEL ENERGY STORAGE APPLIED TO SOLAR ELECTRIC PROPULSION, </b>M. W. Marasch - Air Force Institute of Technology; C. D. Hall - Virginia Polytechnic Institute and State University <li><a href="abstracts/98-205.html"><b>AAS 98-205</b></a> -- <b>OPTIMAL LOW-THRUST TRANSFERS TO HALO ORBITS ABOUT THE L2 LIBRATION POINT IN THE EARTH-MOON SYSTEM (ELLIPTICAL PROBLEM), </b>T. F. Starchville, Jr. - The Aerospace Corporation; R. G. Melton - Pennsylvania State University </ul> <dt><h3>Session 18: Numerical Analysis</h3> <h4>Wednesday, February 11, 1:30 PM / Laguna Ballroom G</h4> <h4>Chair: DR. DONALD L. MACKISON, University of Colorado</h4> <ul> <li><a href="abstracts/98-206.html"><b>AAS 98-206</b></a> -- <b>OPTIMAL BEST FITTING OF NUMERICAL DATA, </b>D. Mortari - Universita degli Studi "La Sapienza" di Roma, Italy <li><a href="abstracts/98-207.html"><b>AAS 98-207</b></a> -- <b>COMPRESSION EPHEMERIDES IN ATTITUDE DYNAMICS, </b>R. Barrio, A. Elipe - Universidad de Zaragoza, Spain; M. Vallejo - Real Observatorio de la Armada, Spain <li><a href="abstracts/98-208.html"><b>AAS 98-208</b></a> -- <b>IMPROVED CHEBYSHEV METHODS FOR THE NUMERICAL INTEGRATION OF FIRST-ORDER DIFFERENTIAL EQUATIONS, </b>D. L. Richardson, D. Schmidt, J. Mitchell - University of Cincinnati <li><a href="abstracts/98-209.html"><b>AAS 98-209</b></a> -- <b>NEW METHODOLOGY FOR SIMULATION VALIDATION AND MODEL MODIFICATION, </b>Li, Xiaolong; Tang, Shuo; Guan, Xiaodong - Northwestern Polytechnical University, P. R. China <li><a href="abstracts/98-210.html"><b>AAS 98-210</b></a> -- <b>TRAJECTORY PROPAGATION USING HIGH-ORDER NUMERICAL INTEGRATORS, </b>G. Der - TRW <li><a href="abstracts/98-211.html"><b>AAS 98-211</b></a> -- <b>ERROR COVARIANCE MATRIX PROPAGATION OVER VERY SHORT TIME SPANS, </b>G. Der - TRW </ul> </dl><P><A HREF="http://www.space-flight.org/AAS_meetings/1998_winter/1998_winter.html">Back</A>