نتایج جستجو برای: robust autopilot

تعداد نتایج: 206741  

Journal: :IBM Systems Journal 2007
Steve Mastrianni David F. Bantz Kirk A. Beaty Tom Chefalas Srikant Jalan Gautam Kar Andrzej Kochut Dong-Jun Lan Larry O'Connell Anca Sailer Gang Wang Qingbo Wang Dennis G. Shea

S. Mastrianni D. F. Bantz K. A. Beaty T. Chefalas S. Jalan G. Kar A. Kochut D. J. Lan L. O’Connell A. Sailer G. Wang Q. B. Wang D. G. Shea IT Autopilot is a flexible architecture to support the delivery of information technology (IT) systems management services. Complex services that involve several tools require integration between the tools and automated processes that can invoke multiple too...

Journal: :Periodicals of Engineering and Natural Sciences (PEN) 2018

Journal: :Systems & Control Letters 2006
Vincent Andrieu Hélène Piet-Lahanier

Interception problems are often dealt with by separating guidance and autopilot design. Guidance law can be obtained using optimal control theory and autopilot design is performed on a linearized system. In this paper, we introduce a new approach that determines a global guidance and autopilot law, based on direct output feedback design. Application of this method to exoatmospheric interception...

2009

Abstract. This paper presents a robust control law design for a commercial aircraft pitch autopilot dedicated to perform the approach maneuver. The design involves only the longitudinal axis. Traditionally, in the aerospace industry, the design of autopilot functions follows a process that involves the partitioning of the flight operational envelope into separate flight conditions, the design o...

Journal: :the modares journal of electrical engineering 2015
somaie dadashi arani ali moarefianpour

this paper presents a gain scheduled autopilot for pitch channel of a flying vehicle. the selected method is based on polynomial fuzzy systems. the method does not involve linearization about operating point. first the polynomial fuzzy model of pitch channel of the flight body is derived. next, using polynomial fuzzy system methodology the controller is design such that the outputs of the nonli...

2005
Chia-Hao Cheng Li-Chen Fu

In this paper, the decision parts of a launch rocket—guidance law (GL) and autopilot—are discussed. In the controller design, the differential geometry and sliding mode control are employed. In addition to the individual GL and autopilot system, stability of the integrated guidance/autopilot (G/A) system are discussed. Finally, various simulations are demonstrated to examine the feasibility and...

Journal: :Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 2011

Journal: :Norsk medietidsskrift 2020

2012
András Molnár

AirGuardian is a complex of an Unmanned Aerial Vehicle and ground station UAV hardware and software systems which has been developed at Obuda University. The hardware and software of the autopilot (AERObot), the antenna tracker station and the ground control station were simultaneously created resulting in the optimal cooperation of the modules. The aim of...

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