Variational Model for Optimization of Finite-Burn Escape Trajectories Using a Direct Method
Trajectory Analysis for the Lunar Flyby Rescue of AsiaSat-3/HGS-1
Finite Burn Maneuver Modeling for a Generalized Spacecraft Trajectory Design and Optimization System
An Architecture for a Generalized Spacecraft Trajectory Design and Optimization System
Indirect Optimization of Low Earth Orbit to Low Lunar Orbit Transfers
Trajectory Optimization With Dual Thrust Limited Propulsion Systems (AAS 01-443)
Geostationary Orbit Transfer using Electric Propulsion for the Hughes HS-702 Satellite
An Efficient Strategy for Targeting Ballistic Lunar Capture Trajectories (AAS 06-129)
Transfers to Earth centered orbits via lunar gravity assist
Direct Multiple Shooting Optimization with Variable Problem Parameters
Decreasing Semimajor Axis Uncertainty Through Trajectory Design (AAS 05-333)
Finite Burn Trajectory Optimization Including Observability With Discrete Measurements (AAS 05-334)
Indirect Optimization of Spiral Trajectories (AAS 05-372)
Incorporating Observability into Trajectory Optimization (AAS 05-132)