Accessibility, Stabilizability, and Feedback Control of Continuous Orbital Transfer
Advanced Stellar Compass: Onboard Autonomous Orbit Determination, Preliminary Performance
A Dynamic Metric for NEO Hazard Mitigation
Analytical Theory of an Artificial Satellite of the Moon
A Roadmap for Optimal Control: The Right Way to Commute
Assessing NEO Hazard Mitigation in Terms of Astrodynamics and Propulsion Systems Requirements
Assessing Potential Propulsion Breakthroughs
A Survey of Propulsion Options for Cargo and Piloted Missions to Mars
A Systematic-Heuristic Approach for Space Trajectory Design
Autonomous Low-Thrust Guidance: Application to SMART-1 and BepiColombo
Canonical Formalism for Modelling and Control of Rigid Body Dynamics
Classification of Periodic Orbits in the Four- and Five-Body Problems
Control of Satellite Clusters in Elliptic Orbit with Limited Communication
Coordinated Orbit Transfer for Satellite Clusters
Decentralized Formation Flying Control in a Multiple-Team Hierarchy
Earth-to-Moon Low Energy Transfers Targeting L~1 Hyperbolic Transit Orbits
Efficient Orbit Integration by Manifold Correction Methods
Existence of Chaos Associated with Weak Ballistic Capture and Applications
ExoMars Alternative Escape Trajectories with Soyuz/Fregat
Finite Burn Maneuver Modeling for a Generalized Spacecraft Trajectory Design and Optimization System
Formation Flying Design and Applications in Weak Stability Boundary Regions
Gauge Freedom in Orbital Mechanics
Geometric Mechanics and the Dynamics of Asteroid Pairs
Hamiltonian Modelling of Relative Motion
Hamilton-Jacobi Modelling of Relative Motion for Formation Flying
Lagrange L~4/L~5 Points and the Origin of Our Moon and Saturn's Moons and Rings
Low Energy Trajectories and Chaos: Applications to Astrodynamics and Dynamical Astronomy
MarsSat: Assured Communication with Mars
Metrics on the Relative Spacecraft Motion Invariant Manifold
Migration of Interplanetary Dust
Migration of Jupiter-Family Comets and Resonant Asteroids to Near-Earth Space
Near-Optimal Reconfiguration and Maintenance of Close Spacecraft Formations
New Orbits for the n-Body Problem
New Trends in Astrodynamics and Applications: Optimal Trajectories for Space Guidance
On the Occurrence of Transition States in Celestial Mechanics
Optimal Plane Changes Using Third-Body Forces
Phobos/Deimos Sample Return via Solar Sail
Recent Gravity-Assist Trajectories for Interplanetary and Solar Exploration
Reduction of Lunar Landing Fuel Requirements by Utilizing Lunar Ballistic Capture
Relative Equilibria for General Gravity Fields in the Sphere-Restricted Full Two-Body Problem
Return Time Dynamics as a Tool for Finding Almost Invariant Sets
Robust Mission Design Through Evidence Theory and Multiagent Collaborative Search
Stability of Relative Equilibria in the Full Two-Body Problem
Teleoperation Support for Early Human Planetary Missions
The Bering Small Vehicle Asteroid Mission Concept