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
LEQG and Game Theoretic Satellite Attitude Control With Magnetic Torquer
On Satellite Umbra/Penumbra Entry and Exit Positions (AAS 97-155)
On the Application of Gravity Gradiometer for Inertial Navigation System
Regularized Equations of Motion for the Alfriend-Coffey Hamiltonian
Further Investigations of the Attitude Motions of a Variable Mass Cylinder
Using the GPS Navigation Solution for Orbit Determination
GPS Navigation Initiatives at Goddard Space Flight Center Flight Dynamics Division
Use of Decoupling Basis Functions in Learning Control for Local Learning and Improved Transients
An Instantaneous Eigenstructure Quasi-Coordinate Formulation for Nonlinear Multibody Dynamics
Preliminary Plans for a Close Encounter With 253 Mathilde
Trajectory Design for a Europa Orbiter Mission: A Plethora of Astrodynamic Challenges
Simultaneous Deployment of a Cable From Two Moving Platforms
Predicting Crack Lengths in Multi-Wall Systems Following a Perforating Orbital Debris Impact
Effects of Exhaust Gases on the Dynamics of Spinning Space Vehicles Undergoing Mass Loss
Short Response Time Options for Impending Asteroid Collision
The Customization of Satellite Tool Kit for Use on the NEAR Mission
Multibody Modeling of Communications Satellite Dynamics for Ground-Based Simulation
Semianalytical Methods for High Eccentric Orbits: Zonal Harmonics and Air Drag Terms
Satellite Orbit Determination Using GPS Pseudoranges Under SA
Near Optimal Control for Flexible Expendable Launch Vehicles
Study on Optimal Filtering for Attitude Determination Applied to the Moon-Sun Sensor
Attitude Determination for Spin Stabilized Satellites from GPS Interferometry
Aerodynamic Stabilization Analysis for LEO Small Satellites