Dynamics modeling and model selection of space debris removal via the Tethered Space Robot
Fuel near-optimal guidance law for the powered descending phase of a lunar module
Fuel near-optimal guidance law for the powered descending phase of a lunar module
Phase Noise Estimation and Suppression for PDM CO-OFDM/OQAM Systems
Linear Parameter-Varying Antiwindup Compensation for Active Microgravity Vibration Isolation
SPECIAL SECTION: DETONATION IN PROPULSION - Detonation in Reactive Solid Particle-Gas Flow
Modal characteristics of a simplified brake rotor model using semi-analytical Rayleigh–Ritz method
Integrated relative position and attitude control of spacecraft in proximity operation missions