Dynamics of vibration isolation system obeying fractional differentiation
Dynamics of vibration isolation system obeying fractional differentiation
A nonlinear stability analysis of elastic flight vehicle
A nonlinear stability analysis of elastic flight vehicle
RDS-SUMO: from lofting to physics-based grids
Collision monitoring and optimal collision avoidance manoeuvre for formation flying satellites
Collision monitoring and optimal collision avoidance manoeuvre for formation flying satellites
Robust performance optimization of dual thrust rocket motor
Development and validation of on-board systems control laws
Development and validation of on-board systems control laws
Optimal formation keeping control in missile cooperative engagement
Optimal formation keeping control in missile cooperative engagement
Attitude cooperative control of spacecraft formation via output-feedback
Attitude cooperative control of spacecraft formation via output-feedback
Stability analysis of aeroelastic systems based on aeroelastic FRF and condition number
Stability analysis of aeroelastic systems based on aeroelastic FRF and condition number
Fuzzy approach for uncertainty analysis of thin walled composite beams
Fuzzy approach for uncertainty analysis of thin walled composite beams
Optimal virtual center selection for formation flying maintenance
Optimal virtual center selection for formation flying maintenance
Dynamics analysis of satellite cluster non-coplanar orbit transfer based on geometric method
Dynamics analysis of satellite cluster non-coplanar orbit transfer based on geometric method
Automated generation of aerofoil characteristics for rotorcraft application
Diesel engine application on AEW&C turboprop effectiveness-cost assessment
Aircraft design using a variable density model
Evaluation on net strength and arresting performance of aircraft arresting system by FE method
Evaluation on net strength and arresting performance of aircraft arresting system by FE method
Integrity monitoring using ERAIM for GNSS/inertial system
Integrity monitoring using ERAIM for GNSS/inertial system
Head-tilt and pilot fatigue measured by flight simulation
Head-tilt and pilot fatigue measured by flight simulation
Structural-aeroelastic finite element modeling for advanced-geometry rotor blades
Structural-aeroelastic finite element modeling for advanced-geometry rotor blades
Investigation on instable current issue of scanning mechanism
Investigation on instable current issue of scanning mechanism