Flight Simulator of Helicopter
Guaranteed Cost Control for Singularly Perturbed Systems under Controller Gain Perturbations
A Polynomial Time Solvable Formulation of Multiple Sequence Alignment
2008-01-1103 Back-Calculated Spindle Loads Sensitivity to Suspension Component Loads Availability
2008-01-1105 Synthesis and Analysis of the Double-Axle Steering Mechanism Considering Dynamic Loads
Quasi-LHD Sequential Sampling Method for Computer Experiments