Adaptive Interplanetary Navigation Using Differenced Range Observables
Aerodynamic Stabilization Analysis for LEO Small Satellites
A Family of Variable-Step Chebyshev Methods for Precise Integration of Perturbed Oscillator Systems
Airborne Kinematic Attitude Determination Using GPS Phase Interferometry
Analysis of Algebraic Solutions to the GPS Navigational Equations
An Instantaneous Eigenstructure Quasi-Coordinate Formulation for Nonlinear Multibody Dynamics
Attitude Determination for Spin Stabilized Satellites from GPS Interferometry
Ballistic Capture Lunar Transfer Determination for the U.S. Air Force Academy Blue Moon Mission
Best Forms of Solution of the Tschauner-Hempel Differential Equations
Conditions for Convergence in Indirect Adaptive Control Based Learning Control
Coordinated Motion Control of Multiple Manipulator Space Free-Flyers
Determination of Optimal Spacecraft Trajectories Using a Step-by-Step Linearization Method
Dynamics and Control of Close Orbits Around Small Rotating Bodies
Dynamics of an Asymmetric Spacecraft Driven by a Constant Thrust: Perturbation Studies
East-West Stationkeeping of Satellite Orbits with Resonant Tesseral Harmonics
Effects of Exhaust Gases on the Dynamics of Spinning Space Vehicles Undergoing Mass Loss
ESOQ-2 Single-Point Algorithm for Fast Optimal Spacecraft Attitude Determination
Experiments Bridging Learning and Repetitive Control
Feedback Time-Optimal Control Synthesis for Flexible Structures With Damping
Further Investigations of the Attitude Motions of a Variable Mass Cylinder
General Form of the Spacecraft Terminal Rendezvous Equations and State Transtion Matrix
GPS Navigation Initiatives at Goddard Space Flight Center Flight Dynamics Division
Improvements in Atmospheric Drag Modeling for Precision Orbit Determination
LEQG and Game Theoretic Satellite Attitude Control With Magnetic Torquer
Lunar and Planetary Missions Launched From a Geosynchronous Transfer Orbit
Mercury Mission Design Using Solar Electric Propulsion Spacecraft
Minimum Time Translation of a Flexible Beam Using Pulse Response Based Control: Experimental Results
Multibody Modeling of Communications Satellite Dynamics for Ground-Based Simulation
Navigation Using Two Angle-Only Measurements to Determine Position of Low-Thrust Spacecraft
Near Optimal Control for Flexible Expendable Launch Vehicles
On Satellite Umbra/Penumbra Entry and Exit Positions (AAS 97-155)
On the Application of Gravity Gradiometer for Inertial Navigation System
On the Possibility of III-Conditioned Covariance Matrices in the First-Order Two-Step Estimator