Vibration Control of Flexible Manipulators Using Smart Structures
Using the GPS Navigation Solution for Orbit Determination
Use of Decoupling Basis Functions in Learning Control for Local Learning and Improved Transients
Trajectory Optimization With Dual Thrust Limited Propulsion Systems
Trajectory Design for a Europa Orbiter Mission: A Plethora of Astrodynamic Challenges
Thermally-Induced Attitude Dynamics of a Spacecraft With a Flexible Boom
The Multiple Spacecraft Orbit Transfer Problem: Case I, No Booster
The Effect of Orbiter-Induced Perturbations on the Trajectory From a Payload Perspective
The Customization of Satellite Tool Kit for Use on the NEAR Mission
Study on Optimal Filtering for Attitude Determination Applied to the Moon-Sun Sensor
Study of Integrated Optimization Method of Trajectory/Vehicle Overall Parameter
Stationkeeping Maneuvers for the China-Brazil Satellite
Staging Point Estimation of a Multi-Stage Launch Vehicle
Space Shuttle Contingency Planning by the Goddard Space Flight Center Flight Dynamics Division
Some Necessary Conditions for the Optimality of Synergetic Maneuvers
Simultaneous Deployment of a Cable From Two Moving Platforms
Short Response Time Options for Impending Asteroid Collision
Semianalytical Methods for High Eccentric Orbits: Zonal Harmonics and Air Drag Terms
Satellite Orbit Determination Using GPS Pseudoranges Under SA
Regularized Equations of Motion for the Alfriend-Coffey Hamiltonian
Preliminary Plans for a Close Encounter With 253 Mathilde
Predicting Crack Lengths in Multi-Wall Systems Following a Perforating Orbital Debris Impact
Performance of TOPEX/POSEIDON "Quick-Look" Precision Orbit Determination in the Extended Mission
Performance Assessment of the Moon-Sun Attitude Sensor
ORB^E~ST - A GPS Navigation Solution Algorithm Without DOP Analysis
On the Possibility of III-Conditioned Covariance Matrices in the First-Order Two-Step Estimator
On the Application of Gravity Gradiometer for Inertial Navigation System
On Satellite Umbra/Penumbra Entry and Exit Positions (AAS 97-155)
Near Optimal Control for Flexible Expendable Launch Vehicles
Navigation Using Two Angle-Only Measurements to Determine Position of Low-Thrust Spacecraft
Multibody Modeling of Communications Satellite Dynamics for Ground-Based Simulation
Minimum Time Translation of a Flexible Beam Using Pulse Response Based Control: Experimental Results
Mercury Mission Design Using Solar Electric Propulsion Spacecraft
Lunar and Planetary Missions Launched From a Geosynchronous Transfer Orbit
LEQG and Game Theoretic Satellite Attitude Control With Magnetic Torquer
Improvements in Atmospheric Drag Modeling for Precision Orbit Determination