FLIGHT MANAGEMENT SYSTEM REQUIREMENT ANALYSIS FOR TRAJECTORY BASED OPERATION
Hovering Formation Design and Control Based on Relative Orbit Elements (AAS 14-377)
Design of Lunar Free-Return Trajectories Based on UKF Parameter Estimation (AAS 14-469)
Collision Avoidance in Elliptical Formation Flying Based on Relative Orbit Elements (AAS 14-208)
Space-Time Coordinate Systems in the High-Precision Orbit Prediction (AAS 14-291)
Optimal Low-Thrust Transfer and Guidance Scheme for Geostationary Orbit Insertion (AAS 14-386)
Reliability Analysis of SGP4 Using GOCE Satellite (AIAA 2014-4281)
Indirect Optimization of Low-Thrust Earth Escape Trajectories (AAS 13-305)
Impulsive Hovering Formation Based on Relative Orbit Elements (AAS 13-395)
Study of Elliptical Relative Motion Control Based on Relative Orbit Elements (AAS 13-474)
Homotopy Method for Minimum Fuel Rendezvous Problem With Gravity Assists (AAS 13-228)
Station-Keeping Strategies for Satellite Constellation (AAS 13-445)
Comparison and Application Analysis of Classical Relative Motion Models (AAS 12-108)
Coverage Analysis of Specified Area for an Agile Earth Observation Satellite (AAS 11-539)
Satellite Relative Motion in Elliptical Orbit Using Relative Orbit Elements (AAS 11-497)
The Implementation of MPI in the Autonomous Navigation of Constellation (AAS 11-545)
Perturbation Effects on Elliptical Relative Motion Based on Relative Orbit Elements (AAS 12-148)
Research of the Free-Return Trajectories between the Earth-Moon (AAS 11-457)