Xiaoli Bai

Latest

• Limits of Machine Learning Approach on Improving Orbit Prediction Accuracy
• Output-Feedback Stochastic Model Predictive Control for Glideslope Tracking During Aircraft Carrier Landing
• Covariance Fusion Method of Gaussian Processes Covariance and Orbital Prediction Uncertainty (Accepted)
• Gaussian Processes for Improving Orbit Prediction Accuracy
• Machine Learning Approach to Improve Satellite Orbit Prediction Accuracy Using Publicly Available Data
• A K Nearest Neighborhood-Based Wind Estimation for Rotary-Wing VTOL UAVs
• Comparative Evaluation of Three Machine Learning Algorithms on Improving Orbit Prediction Accuracy (Accepted)
• Modeling and Simulation of UAV Carrier Landings
• Natural Deep Space Satellite Constellation in the Earth-Moon Elliptic System
• Comparison of Effective Machine Learning Algorithms on Improving Orbit Prediction Accuracy
• Artificial Neural Network–Based Machine Learning Approach to Improve Orbit Prediction Accuracy
• Quadrotor Autonomous Approaching and Landing on a Vessel Deck
• Generalization Capability of Machine Learning Approach Among Different Satellites: Validated Using TLE Data
• Obtain Confidence Interval for the Machine Learning Approach to Improve Orbit Prediction Accuracy
• Exploring Capability of Support Vector Machine for Improving Satellite Orbit Prediction Accuracy
• A Machine Learning Approach to Improve Satellite Orbit Prediction Accuracy: Validation Using Publicly Available Data
• Improving Orbit Prediction Accuracy Through Supervised Machine Learning
• Halo Orbit Station-Keeping Using Nonlinear MPC and Polynomial Optimization
• Recovering Area-to-Mass Ratio of Resident Space Objects through Data Mining
• Using Artificial Neural Network in Machine Learning Approach to Improve Orbit Prediction Accuracy
• Libration Transfer Design Using Patched Elliptic Three-Body Models and Graphics Processing Units
• Continuation of Periodic Orbits in the Sun-Mercury Elliptic Restricted Three-Body Problem
• Efficient and Adaptive Orthogonal Finite Element Representation of the Geopotential
• New Natural Formation Flying Configurations in the Earth-Moon Elliptic Three-Body System
• Finite-Time Control for Asteroid Hovering and Landing via Terminal Sliding-Mode Guidance
• Maintenance of Libration Point Orbit in Elliptic Sun-Mercury Model
• Optimal Path Planning for Free-Flying Space Manipulators via Sequential Convex Programming
• Rapid Generation of Time-Optimal Trajectories for Asteroid Landing via Convex Optimization
• Rapid Trajectory Planning for Asteroid Landing with Thrust Magnitude Constraint
• Task-Constrained Trajectory Planning of Free-Floating Space-Robotic Systems Using Convex Optimization
• Picard Iteration, Chebyshev Polynomials and Chebyshev-Picard Methods: Application in Astrodynamics
• Modified Chebyshev-Picard Iteration Methods for Solution of Initial Value Problems
• Modified Chebyshev-Picard Iteration Methods for Station-Keeping of Translunar Halo Orbits
• Orthogonal Approximation in Higher Dimensions: Applications in Astrodynamics
• Tangent Orbital Rendezvous with the Same Direction of Terminal Velocities
• Modified Chebyshev-Picard Iteration Methods for Orbit Propagation
• Modified Chebyshev-Picard Iteration Methods for Solution of Boundary Value Problems
• Modified Chebyshev-Picard Iteration Methods for Solution of Initial Value and Boundary Value Problems
• Solving Initial Value Problems by the Picard-Chebyshev Method with NVIDIA GPUs
• Bang-Bang Control Design by Combing Pseudospectral Method with a Novel Homotopy Algorithm
• New Results for Time-Optimal Three-Axis Reorientation of a Rigid Spacecraft
• Dynamic Analysis and Control of a Stewart Platform Using A Novel Automatic Differentiation Method