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Orbit phasing

  • Astrodynamics

    Astrodynamics

  • Evolution of the Rendezvous-Maneuver Plan for Lunar-Landing Missions

    Evolution of the Rendezvous-Maneuver Plan for Lunar-Landing Missions

  • Low Earth Orbit Slotting for Space Traffic Management Using Flower

    Low Earth Orbit Slotting for Space Traffic Management Using Flower

  • Lunar Orbiting Cubesat Sensor Transport System Mike Seibert, Alejandro Levi, and Mitchell Paradis Graduate Students, Colorado School of Mines

    Lunar Orbiting Cubesat Sensor Transport System Mike Seibert, Alejandro Levi, and Mitchell Paradis Graduate Students, Colorado School of Mines

  • ISTS-2017-D-110ⅠISSFD-2017-110

    ISTS-2017-D-110ⅠISSFD-2017-110

  • Advantages of Small Satellite Carrier Concepts for LEO/GEO Inspection and Debris Removal Missions

    Advantages of Small Satellite Carrier Concepts for LEO/GEO Inspection and Debris Removal Missions

  • INPOP08, a 4-D Planetary Ephemeris: from Asteroid and Time-Scale Computations to ESA Mars Express and Venus Express Contributions

    INPOP08, a 4-D Planetary Ephemeris: from Asteroid and Time-Scale Computations to ESA Mars Express and Venus Express Contributions

  • Ssc15-Viii-1

    Ssc15-Viii-1

  • Guidance, Navigation, and Control for Commercial and Scientific Applications of Formation Flying

    Guidance, Navigation, and Control for Commercial and Scientific Applications of Formation Flying

  • Orbital Mechanics, Oxford University Press

    Orbital Mechanics, Oxford University Press

  • Aas 19-221 Modern Aerocapture Guidance to Enable Reduced-Lift Vehicles at Neptune

    Aas 19-221 Modern Aerocapture Guidance to Enable Reduced-Lift Vehicles at Neptune

  • Valuation of On-Orbit Servicing in Proliferated Low-Earth Orbit Constellations

    Valuation of On-Orbit Servicing in Proliferated Low-Earth Orbit Constellations

  • Geosynchronous Earth Orbit/Low Earth

    Geosynchronous Earth Orbit/Low Earth

  • Phases and Manoeuvres Involved in Orbital Rendezvous Missions

    Phases and Manoeuvres Involved in Orbital Rendezvous Missions

  • Active Removal of Space Debris Expanding Foam Application for Active Debris Removal

    Active Removal of Space Debris Expanding Foam Application for Active Debris Removal

  • Electric Propulsion for Small Satellites: a Case Study

    Electric Propulsion for Small Satellites: a Case Study

  • Earth Orbit Raise Design for the ARTEMIS Mission

    Earth Orbit Raise Design for the ARTEMIS Mission

  • Aas 19-233 Mars Reconnaissance Orbiter Maneuver Plan for Mars 2020 Entry, Descent, and Landing Support and Beyond

    Aas 19-233 Mars Reconnaissance Orbiter Maneuver Plan for Mars 2020 Entry, Descent, and Landing Support and Beyond

Top View
  • On-Orbit Serviceability of Space System Architectures
  • Techniques for Leo Constellation Deployment and Phasing Utilizing Differential Aerodynamic Drag
  • A Framework for Efficient Trajectory Comparisons in the Earth-Moon Design Space
  • Propellantless Space Travel Using Recycled Kinetic Energy (Pdf, 733K)
  • 2019 Astrodynamics Specialist Conference Portland, ME, August 11-15, 2019 Aug 12, 2019 Hawthorne
  • Microsat Constellation Control Techniques
  • Aas 15-456 Trajectory Design from Gto to Near-Equatorial Lunar Orbit for the Dark Ages Radio Explorer (Dare) Spacecraft
  • Orbit Determination and Differential-Drag Control of Planet Labs Cubesat Constellations
  • Fast Low Earth Orbit Acquisition Plan Optimiser
  • 1 the LUNAR ORBIT PHASING and RENDEZVOUS TESTS of CHANG
  • The Impact of Maneuver Failures on the Eos Afternoon Constellation
  • Trajectory Optimization and Control of Small Spacecraft Constellations by Emmanuel Joseph Sin a Dissertation Submitted in Partia
  • Parallel High-Fidelity Trajectory Optimization with Application to Cubesat Deployment in an Earth-Moon Halo Orbit
  • Characteristics of the Flank Magnetopause: THEMIS Observations
  • Virtual Formation Method for Precise Autonomous Absolute Orbit Control
  • D2.1 VLEO Aerodynamics Requirements Document
  • An Updated Re-Entry Analysis of the Hubble Space Telescope
  • IEEE AC 2014 Paper 2464 Bester ARTEMIS Operations 20140310 Final


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