Nonlinear μ Flight Control and Suboptimal Exact Solution on F-16 Application | 0 | 0.34 | 2005 |
Mixed H2/H∞ attitude control of a LEO microsatellite in the presence of inertia matrix uncertainty | 1 | 0.42 | 2002 |
Nonlinear H∞ robust control for satellite large angle attitude maneuvers | 0 | 0.34 | 2001 |