Academic
Publications
Feedback Control of Dynamic Systems

Feedback Control of Dynamic Systems,G. F. Franklin,J. D. Powell,A. Emani-naeini

Feedback Control of Dynamic Systems   (Citations: 1013)
BibTex | RIS | RefWorks Download
Published in 1994.
Cumulative Annual
    • ...Available results in the particular framework of SD systems show that significant improvement in control performance can be achieved when the so-called direct design of digital controller for continuous-time process is adopted (Chen and Patton 1999; Franklin, Powell, and Emami-Naeini 2002)...

    M. L. Corradiniet al. Design of robust fault detection filters for MIMO uncertain plants wit...

    • ...Thum, Du, Chen, Ong, and Tan (2008) and Piskorowski (2010) have proposed linear time-varying (LTV) filters with varying filter gain and damping ratio (or quality factor Q in communications and filter engineering (Franklin, Powell, and Emami-Naeini 2002))...

    Fan Honget al. A peak filtering method with improved transient response for narrow-ba...

    • ...The design of a linear full-order estimator, as described in [16], starts with a linear system in state-space form...

    Chris Satkoskiet al. Piezoelectric Fuel Injection: Pulse-to-Pulse Coupling and Flow Rate Es...

    • ...In simulations, we use the linearized lateral dynamics model of a Boeing 747 airplane [13] as the controlled plant...
    • ...The aircraft model [13] is modified with two augmented actuation vectors b2u2 and b3u3, for the study of actuator failure compensation...
    • ...represent three rudder servos’ angles: δr1, δr2, δr3, from a three-piece rudder with needed redundancy for achieving failure compensation in the presence of actuator failures (the no-redundancy case [13] is with for u1 = δr, the single rudder servo angle, while u2 = u3 = 0)...
    • ...According the data of horizontal flight 40,000 ft and nominal forward speed 774 ft/sec (Mach 0.8), which provided in [13], we obtain the discrete-time model of the Boeing 747 lateral-perturbation dynamics with sampling time T = 0.1s...

    Chang Tanet al. A discrete-time parameter estimation based adaptive actuator failure c...

    • ...As an alternative to Bode diagrams, Nyquist plots are more suitable to analyze complex systems in which the magnitude and phase curves may cross, respectively, 0 dB or 180 deg several times [41]...
    • ...The error rejection can be quantified through the sensitivity function as [41], [50]...
    • ...According to the Nyquist theory, the system is stable if and only if its trajectory does not encircle the critical point (−1, 0j) [1], [3], [41], [42], [51]...

    Alejandro G. Yepeset al. Analysis and Design of Resonant Current Controllers for Voltage-Source...

Sort by: