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A sigma-point batch filter for spacecraft orbit estimation using the geomagnetic field measurements
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Optimal Formation Reconfigurations subject to Hill Three-Body Dynamics
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Hardware-in-the-loop simulations of spacecraft attitude synchronization using the state-dependent Riccati equation technique
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Integrated Orbit and Attitude Hardware-in-the-Loop Simulations for Autonomous Satellite Formation Flying
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Spacecraft Fuel-Optimal and Balancing Maneuvers for a Class of Formation Reconfiguration Problems
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Analytical Solution to Optimal Relocation of Satellite Formation Flying in Arbitrary Elliptic Orbits
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Necessary Conditions for the Optimality of Singular Arcs of Spacecraft Trajectories Subject to Multiple Gravitational Bodies
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Spacecraft Attitude Control via a Combined State-Dependent Riccati Equation and Adaptive Neuro-Fuzzy Approach
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Linearized Dynamics Model for Satellite Relative Motion under a J2-Perturbed Elliptical Reference Orbit
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Non-Recursive Estimation Using a Batch Filter Based on Particle Filtering
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Integrated Attitude Determination and Control System via Magnetic Measurements and Actuation
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Analytic Solution to Optimal Reconfigurations of Satellite Formation Flying in Circular Orbit under J2 Perturbation
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Simultaneous Spacecraft ?Attitude and Orbit Estimation Using ?Magnetic Field Vector Measurements
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Satellite Formation Reconfiguration and Station Keeping Using State-Dependent Riccati Equation Technique
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Sigma – Point Kalman Filtering for Spacecraft ?Attitude and Rate Estimation Using ?Magnetometer Measurements
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Ground vehicle navigation in harsh urban conditions by integrating inertial navigation system, global positioning system, odometer and vision data
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Magnetic Torque Attitude Control of a Satellite Using the State-Dependent Riccati Equation Technique
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Approximate Analytical Solutions to Optimal Reconfiguration Problems in Perturbed Satellite Relative Motion
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High-Accuracy Trajectory Optimization for a Trans-Earth Lunar Mission
