نتایج جستجو برای: model helicopter

تعداد نتایج: 2107554  

, H. Zamani and S. Ziaiee Rad,

An approximate numerical mthod is presented for analysis and determination of modal characteristics in straight, pretwisted non-unifom helicopter blades. The analysis considers the coupled flapwise bending (out of plane), chordwise bending (in plane), and torsion vibration of both rotating and non-rotating blades. The proposed method is based on the integral expansion of Green functions (struct...

1988
Thomas P. Hamilton

An expert system for diagnosing faults in the power train of a twin-engine gas turbine helicopter has been developed. The system, designated HELIX (HELicopter Integrated expert), performs diagnostic reasoning based on a hierarchical qualitative model representing the major power train components and the physical principles that govern their interaction. The approach represents a promising techn...

2004
Jagath C. Rajapakse Kunihiko Fukushima Soo-Young Lee S. Suresh M. Vijaya Kumar Omkar V. Mani Prasad Sampath

In this paper, identification of lateral and longitudinal dynamics of helicopter using flight data is presented. Neural networks with linear filter also known as Narendra's model and recurrent neural networks with intemal memory (Memory Neuron Networks) are used for the purpose. These networks are used for identifying the rate and attitude response of the helicopter to a given longitudinal cycl...

2012
S. A. Currie

An auto-pilot system was created which could track and control a Syma S107 RC mini infrared helicopter in real-time. The helicopter was tracked using two LEDs attached to it, one situated on the front of the helicopter and one situated on the tail. Image processing and object tracking algorithms were used to track the position of the helicopter. In order to perform real-time tracking, the metho...

2012
Sergio Esteban Rafael Vazquez Francisco Gordillo Javier Aracil

This paper presents a singular perturbation stability analysis for a nonlinear three-time-scale autonomous helicopter model in vertical flight. The presented time-scale analysis permits to conduct a stability analysis for the singular perturbed threetime-scale system, and allows to construct a composite Lyapunov function for the resultant closed-loop system using time-scale separation. The meth...

2014
Ali Punjani Pieter Abbeel

Machine Learning for Helicopter Dynamics Models by Ali Punjani Master of Science in Computer Science University of California, Berkeley Professor Pieter Abbeel, Chair We consider the problem of system identification of helicopter dynamics. Helicopters are complex systems, coupling rigid body dynamics with aerodynamics, engine dynamics, vibration, and other phenomena. Resultantly, they pose a ch...

Journal: :Journal of Aerospace Science and Technology 2016

Journal: :IEEE transactions on neural networks 2003
Russell Enns Jennie Si

This paper advances a neural-network-based approximate dynamic programming control mechanism that can be applied to complex control problems such as helicopter flight control design. Based on direct neural dynamic programming (DNDP), an approximate dynamic programming methodology, the control system is tailored to learn to maneuver a helicopter. The paper consists of a comprehensive treatise of...

Journal: :International Journal of Control Science and Engineering 2012

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