Zobrazeno 1 - 10
of 11
pro vyhledávání: '"Tony M. Adami"'
Publikováno v:
2014 IEEE/AIAA 33rd Digital Avionics Systems Conference (DASC).
Publikováno v:
IFAC Proceedings Volumes. 34:326-331
Aerospace engineering experiments are made accessible via internet for education purposes within a team of universities in Europe and Amerika. The students at the partner institutes perform by telematic techniques at their home university the experim
Autor:
J. Jim Zhu, Tony M. Adami
Publikováno v:
Proceedings of the 2011 American Control Conference.
In this paper, Trajectory Linearization Control (TLC) is used to design a six degree-of-freedom, autonomous, trajectory-tracking controller for a fixed-wing vehicle dynamics model. TLC combines an open-loop dynamic inverse of the plant dynamics with
Publikováno v:
IFAC Proceedings Volumes. 34:471-473
Since early in the 1990's, the control systems research group at Ohio University has been developing and operating a flexible-structure test facility called Flexlab, and the facility is now available for use via the World Wide Web. Using position and
Publikováno v:
SPIE Proceedings.
This paper discusses a sensor simulator/synthesizer framework that can be used to test and evaluate various sensor integration strategies for the implementation of an External Hazard Monitor (EHM) and Integrated Alerting and Notification (IAN) functi
Publikováno v:
AIAA Infotech@Aerospace Conference.
In this paper, we present a modeling error driven adaptive controller for control of a robot with unknown dynamics. In general, modeling error is not used since the ideal parameters are not known. However, using a feedback linearization approach we s
Autor:
Tony M. Adami, J. Jim Zhu
Publikováno v:
AIAA Guidance, Navigation and Control Conference and Exhibit.
[Abstract] Trajectory Linearization Control (TLC) has been used in recent years to synthesize rigid-body flight controllers with excellent results. However, current scramjet vehicle models feature long, slender fuselages, and integrated engine/airfra
Publikováno v:
AIAA Guidance, Navigation, and Control Conference and Exhibit.
An analytical "loss of stability" indicator is presented which can be applied to complex nonlinear time-varying systems of arbitrary order. The authors propose the use of the Lyapunov Exponent as a "departure index" which can be especially useful in
Publikováno v:
22nd Digital Avionics Systems Conference Proceedings (Cat No 03CH37449) DASC-03.
Vibration due to flexible modes can be attenuated using a notch filter tuned at the known resonant frequencies of a flexible structure or vehicle. However, there are applications in which those particular resonant frequencies are not known a priori.
Autor:
R. Dennis Irwin, Tony M. Adami
Publikováno v:
AIAA Guidance, Navigation, and Control Conference and Exhibit.
State-space models with block-diagonal system matrices allow for straightforward control system design. Often, however, methods to block-diagona lize suffer from numerical instabilities. The author investigates a technique that would obtain such mode