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)
Comparison and Application Analysis of Classical Relative Motion Models (AAS 12-108)
Design of Lunar Free-Return Trajectories Based on UKF Parameter Estimation (AAS 14-469)
Satellite Relative Motion in Elliptical Orbit Using Relative Orbit Elements (AAS 11-497)
Coverage Analysis of Specified Area for an Agile Earth Observation Satellite (AAS 11-539)
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)
Examination of SGP4 Accuracy in Orbit Prediction Using the CHAMP Satellite (AAS 11-172)
Optimization of Hybrid-Orbit Constellation Servicing for Constellations (AAS 11-228)
Nonlinear Control to Attitude Acquisition of Gravitational Stabilized Small-Satellites
Performance History and Prediction Modeling for Minnesota Pavements
Design of Guidance Laws for Lunar Pinpoint Soft Landing (AAS 09-431)
Homotopy Method for Minimum Fuel Rendezvous Problem With Gravity Assists (AAS 13-228)
The Implementation of MPI in the Autonomous Navigation of Constellation (AAS 11-545)