Variable Structure Output Feedback Control of a Spacecraft Under Input Dead-Zone Non-Linearity
Adaptive Variable Structure and Commanding Shaped Vibration Control of Flexible Spacecraft
Variable structure output feedback control of a spacecraft under input dead-zone non-linearity
Optimal sliding mode manoeuvring control and active vibration reduction of flexible spacecraft
Optimal Sliding Mode Manoeuvring Control and Active Vibration Reduction of Flexible Spacecraft
ENGINEERING NOTES - Vibration Suppression of Flexible Spacecraft During Attitude Maneuvers
The Comparative Study on the Sustainable Sites Indicators between ESGB and LEED
MODELLING OF DYNAMIC RESPONSES OF AN AUTOMOTIVE FUEL RAIL SYSTEM, PART I: INJECTOR
Frequency Chirp Supported Complex Modulation of Directly Modulated Lasers (Top-Scored)
ICAS2016_0221: SECURE ESTIMATION FOR UNMANNED AERIAL VEHICLES AGAINST ADVERSARIAL ATTACKS
A ``Reality Vision'' Navigation Technique Based on Sequence Geo-Referenced Image Databases