Navigation Using Two Angle-Only Measurements to Determine Position of Low-Thrust Spacecraft
The Multiple Spacecraft Orbit Transfer Problem: Case I, No Booster
Vibration Control of Flexible Manipulators Using Smart Structures
Determination of Optimal Spacecraft Trajectories Using a Step-by-Step Linearization Method
Analysis of Algebraic Solutions to the GPS Navigational Equations
Mercury Mission Design Using Solar Electric Propulsion Spacecraft
Ballistic Capture Lunar Transfer Determination for the U.S. Air Force Academy Blue Moon Mission
Conditions for Convergence in Indirect Adaptive Control Based Learning Control
Dynamics and Control of Close Orbits Around Small Rotating Bodies
Space Shuttle Contingency Planning by the Goddard Space Flight Center Flight Dynamics Division
ORB^E~ST - A GPS Navigation Solution Algorithm Without DOP Analysis
Staging Point Estimation of a Multi-Stage Launch Vehicle
On the Possibility of III-Conditioned Covariance Matrices in the First-Order Two-Step Estimator
Performance of TOPEX/POSEIDON "Quick-Look" Precision Orbit Determination in the Extended Mission