2037 - 2051 |
Quantifying the accuracy of Hammerstein model estimation Ninness B, Gibson S |
2053 - 2062 |
Stabilizing underwater vehicle motion using internal rotors Woolsey CA, Leonard NE |
2063 - 2073 |
Nonlinear tracking control in the presence of state and control constraints: a generalized reference governor Gilbert E, Kolmanovsky I |
2075 - 2084 |
Robust decentralized stabilization for a class of large-scale time-delay uncertain impulsive dynamical systems Guan ZH, Chen GR, Yu XH, Qin Y |
2085 - 2092 |
Some applications of randomized algorithms for control system design Patel VV, Deodhare G, Viswanath T |
2093 - 2102 |
Constrained receding horizon predictive control for nonlinear systems Lee YI, Kouvaritakis B, Cannon M |
2103 - 2109 |
Repetitive control for systems with uncertain period-time Steinbuch M |
2111 - 2119 |
Controller performance benchmarking and tuning using generalised minimum variance control Grimble MJ |
2121 - 2125 |
Numerically reliable design for proportional and derivative state-feedback decoupling controller Chu DL, Malabre M |
2127 - 2137 |
Closed-loop identification with an unstable or nonminimum phase controller Codrons B, Anderson BDO, Gevers M |
2139 - 2146 |
Analysis of discrete-time piecewise affine and hybrid systems Ferrari-Trecate G, Cuzzola FA, Mignone D, Morari M |
2147 - 2152 |
Matching, linear systems, and the ball and beam Andreev F, Auckly D, Gosavi S, Kapitanski L, Kelkar A, White W |
2153 - 2158 |
Hybrid state estimation: a target tracking application Boers Y, Driessen H |
2159 - 2167 |
Non-singular terminal sliding mode control of rigid manipulators Feng Y, Yu XH, Man ZH |
2169 - 2175 |
Velocity observers for non-linear mechanical systems subject to non-smooth impacts Menini L, Tornambe A |
2177 - 2184 |
Piecewise-affine Lyapunov functions for discrete-time linear systems with saturating controls Milani BEA |
2185 - 2187 |
Nyquist stability criterion of intrinsic zeros for continuous-time pure imaginary zeros Ishitobi M, Kashiwamoto K |
2189 - 2189 |
Comments on "Fully magnetic attitude control for spacecraft subject to gravity gradient" Damaren CJ |