Zobrazeno 1 - 10
of 14
pro vyhledávání: '"Shu-Nan Wu"'
Publikováno v:
Sensors, Vol 13, Iss 4, Pp 4742-4759 (2013)
In this paper, an adaptive law with an integral action is designed and implemented on a DC motor by employing a rotary encoder and tachometer sensors. The stability is proved by using the Lyapunov function. The tracking errors asymptotically converge
Externí odkaz:
https://doaj.org/article/b651832c087b4637a2c93b50b29746d4
Publikováno v:
The Scientific World Journal, Vol 2013 (2013)
The robust H∞ control for spacecraft rendezvous with a noncooperative target is addressed in this paper. The relative motion of chaser and noncooperative target is firstly modeled as the uncertain system, which contains uncertain orbit parameter an
Externí odkaz:
https://doaj.org/article/6da04b42cd654535a4c102aefbf353c9
Publikováno v:
Asian Journal of Control. 19:787-791
This paper investigates the exponential stability problem for a class of multi-area power systems with time delays under load frequency controller failures LFCFs. For describing the phenomenon of LFCFs, the considered multi-area power system is rewri
Publikováno v:
Mathematical Problems in Engineering. 2013, p1-7. 7p.
Publikováno v:
Sensors, Vol 13, Iss 4, Pp 4742-4759 (2013)
Sensors (Basel, Switzerland)
Sensors
Volume 13
Issue 4
Pages 4742-4759
Sensors (Basel, Switzerland)
Sensors
Volume 13
Issue 4
Pages 4742-4759
In this paper, an adaptive law with an integral action is designed and implemented on a DC motor by employing a rotary encoder and tachometer sensors. The stability is proved by using the Lyapunov function. The tracking errors asymptotically converge
Publikováno v:
Aerospace Science and Technology. 25:102-113
Coordinated control problem of translation and rotation between two spacecraft is investigated in this paper. Using dual quaternion, we establish the relative coupled dynamic model in which the coupling effect between translational and rotational mot
Publikováno v:
Applied Mechanics and Materials. :847-851
The attitude maneuver control of flexible spacecraft with finite-time convergence is investigated in this paper. Two terminal sliding mode controllers are proposed to achieve the finite-time control, which guarantee the convergence of attitude maneuv
Publikováno v:
ICCA
Communication systems of formation micro-satellites involve a variety of algorithms and models. In this paper we establish the communication systems modeling TTDPN (T-Timed Discrete Petri Net) of formation small satellites, and establish the map betw
Publikováno v:
Mathematical Problems in Engineering, Vol 2013 (2013)
Robust finite-time control for spacecraft with coupled translation and attitude dynamics is investigated in the paper. An error-based spacecraft motion model in six-degree-of-freedom is firstly developed. Then a finite-time controller based on nonsin