Spaceflight dynamics 1993; AAS/NASA International Symposium, 8th, Greenbelt, MD, Apr. 26-30, 1993, Parts 1 & 2A conference on spaceflight dynamics produced papers in the areas of orbit determination, spacecraft tracking, autonomous navigation, the Deep Space Program Science Experiment Mission (DSPSE), the Global Positioning System, attitude control, geostationary satellites, interplanetary missions and trajectories, applications of estimation theory, flight dynamics systems, low-Earth orbit missions, orbital mechanics, mission experience in attitude dynamics, mission experience in sensor studies, attitude dynamics theory and simulations, and orbit-related experience. These papaers covered NASA, European, Russian, Japanese, Chinese, and Brazilian space programs and hardware.
Teles, Jerome (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Samii, Mina V. (Computer Sciences Corp. Lanham-Seabrook, MD, United States)
August 16, 2013
January 1, 1993
IDRelationTitle19950054162Analytic SubsidiaryOptimum transfer to a large-amplitude halo orbit for the Solar and Heliospheric Observatory (SOHO) spacecraft19950054163Analytic SubsidiaryControl of libration point orbits using lunar gravity-assisted transfer19950054166Analytic SubsidiaryH(sub infinity)-type filter for spacecraft attitude estimation19950054179Analytic SubsidiarySolar flux forecasting using mutual information with an optimal delay19950054202Analytic SubsidiaryFast Auroral Snapshot performance using a multi-body dynamic simulation19950054130Analytic SubsidiaryTargeting an asteroid: The DSPSE encounter with asteroid 1620 Geographos19950054135Analytic SubsidiaryPrecision orbit determination using TOPEX/Poseidon TDRSS observations19950054125Analytic SubsidiaryPrecise navigation for the Earth Observing System (EOS)-AM1 spacecraft using the TDRSS Onboard Navigation System (TONS)19950054175Analytic SubsidiaryReentry analysis for low Earth orbiting spacecraft19950054206Analytic SubsidiaryAtlas IIAS ascent trajectory design for the SOHO mission19950054148Analytic SubsidiaryDetermination and characterization of the Hubble Space Telescope pointing stability19950054165Analytic SubsidiaryKalman filter estimation of attitude and gyro bias with the QUEST observation model19950054133Analytic SubsidiaryComparison of TOPEX/Poseidon orbit determination solutions obtained by the Goddard Space Flight Center Flight Dynamics Division and Precision Orbit Determination Teams19950054208Analytic SubsidiaryThe effect of high lift to drag ratio on aerobraking19950054193Analytic SubsidiaryPostlaunch calibration of spacecraft attitude instruments19950054136Analytic SubsidiaryConservative force model performance for TOPEX/Poseidon precision orbit determination19950054212Analytic SubsidiaryTransfer trajectories for distant retrograde orbiters of the Earth19950054118Analytic SubsidiaryPrecision X-band Doppler and ranging navigation for current and future Mars exploration missions19950054124Analytic SubsidiaryPerformance assessment of the TDRSS Onboard Navigation System (TONS) experiment on EP/EUVE19950054119Analytic SubsidiaryApplication of high precision two-way S-band ranging to the navigation of the Galileo Earth encounters19950054128Analytic SubsidiaryTrajectory design for the Deep Space Program Science Experiment (DSPSE) mission19950054194Analytic SubsidiaryLost in space: Onboard star identification using CCD star tracker data without an a priori attitude19950054170Analytic SubsidiaryExtreme Ultraviolet Explorer attitude determination support with a multimission three-axis stabilized spacecraft flight dynamics support system19950054143Analytic SubsidiaryImpact of suntracking on Space Station controllability19950054129Analytic SubsidiaryOrbit determination covariance analysis for the Deep Space Program Science Experiment mission19950054187Analytic SubsidiaryUpper Atmosphere Research Satellite attitude disturbances during shadow entry and exit19950054141Analytic SubsidiaryU.S. Space Shuttle GPS navigation capability for all mission phases19950054134Analytic SubsidiaryPrecision orbit determination using the Tracking and Data Relay Satellite System (TDRSS)19950054197Analytic SubsidiaryNew dynamic variables for rotating spacecraft19950054177Analytic SubsidiaryInteractive method for planning constrained, fuel-optimal orbital proximity operationsvisibility_off