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Spacecraft Attitude Control via a Combined State-Dependent Riccati Equation and Adaptive Neuro-Fuzzy Approach
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Attitude Synchronization of the Spacecraft Formation Flying via The SDRE Controller Using Reaction Wheels
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Optimal Guidance of Tetrahedral Satellite Formation
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Second-Order Analytical Solution to Fuel-Optimal Control Problems in Satellite Formation Flying
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Analysis for chain-crash risk of LEO satellite due to collision between Iridium-33 and Cosmos-2251
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Laboratory Experiments for Validating the Spacecraft Attitude Control Laws
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Development of Spaceborne GPS Receiver with Real-time Orbit Determination using Unscented Kalman Filter
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Integrated Attitude Determination and Control System via Magnetic Measurements and Actuation
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A Hardware-in-the-loop Simulations for GPS based Formation Navigation and Control 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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Optimal Control and Hamiltonian Dynamics
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Spacecraft Formation Flying with an Earth-Crossing Object for Earth Impact Avoidance
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The Relaxed State-Dependent Riccati Equation Technique: Concept and Applications
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Fuel-Optimal Design of Moon-Earth Trajectories Using Legendre Pseudospectral Method
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Lunar Cargo Mission Design Strategy Using Variable Low Thrust
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Simple Analytic Solution to the Optimal Reconfigurations in General Relative Motions
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Simultaneous Spacecraft Attitude and Orbit Estimation Using Magnetic Field Vector Measurements
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Nonlinear Attitude Dynamics and Control for Satellite Tethered Formation Flying in Three Dimensional Free Space
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The Reconfiguration and Formation-Keeping with State-Dependent Riccati Equation Nonlinear Controller
