An overview on development of miniature unmanned rotorcraft systems

G Cai, BM Chen, TH Lee - … of Electrical and Electronic Engineering in …, 2010 - Springer
In this article, we attempt to document a technical overview on modern miniature unmanned
rotorcraft systems. We first give a brief review on the historical development of the rotorcraft …

[图书][B] Modelling and control of mini-flying machines

P Castillo, R Lozano, AE Dzul - 2005 - books.google.com
Problems in the motion control of aircraft are of perennial interest to the control engineer as
they tend to be of complex and nonlinear nature. Modelling and Control of Mini-Flying …

[图书][B] Identification modeling and characteristics of miniature rotorcraft

B Mettler - 2013 - books.google.com
Identification Modeling and Characteristics of Miniature Rotorcraft introduces an approach to
developing a simple and effective linear parameterized model of vehicle dynamics using the …

Flapping flight for biomimetic robotic insects: Part II-flight control design

X Deng, L Schenato, SS Sastry - IEEE transactions on robotics, 2006 - ieeexplore.ieee.org
In this paper, we present the design of the flight control algorithms for flapping wing
micromechanical flying insects (MFIs). Inspired by the sensory feedback and neuromotor …

A survey and categorization of small low-cost unmanned aerial vehicle system identification

NV Hoffer, C Coopmans, AM Jensen… - Journal of Intelligent & …, 2014 - Springer
Remote sensing has traditionally be done with satellites and manned aircraft. While these
methods can yield useful scientific data, satellites and manned aircraft have limitations in …

Mathematical modeling and experimental identification of an unmanned helicopter robot with flybar dynamics

SK Kim, DM Tilbury - Journal of robotic systems, 2004 - Wiley Online Library
This paper presents a mathematical model for a model‐scale unmanned helicopter robot,
with emphasis on the dynamics of the flybar. The interaction between the flybar and the main …

Robust feedback linearization and GH/sub/spl infin//controller for a quadrotor unmanned aerial vehicle

A Mokhtari, A Benallegue… - 2005 IEEE/RSJ …, 2005 - ieeexplore.ieee.org
In this paper, a mixed robust feedback linearization with linear GH controller is applied to a
non linear quadrotor unmanned aerial vehicle. An actuator saturation and constrain on state …

Dynamic modelling and experimental identification of four rotors helicopter parameters

L Derafa, T Madani… - 2006 IEEE international …, 2006 - ieeexplore.ieee.org
In this paper an experimental identification of dynamic parameters of a four rotors mini
helicopter is presented. An appropriate model for identification and control synthesis is …

Approaches for a tether-guided landing of an autonomous helicopter

SR Oh, K Pathak, SK Agrawal, HR Pota… - IEEE Transactions on …, 2006 - ieeexplore.ieee.org
In this paper, we address the design of an autopilot for autonomous landing of a helicopter
on a rocking ship, due to rough sea. A tether is used for landing and securing a helicopter to …

Flight control of a rotary wing UAV using backstepping

B Ahmed, HR Pota, M Garratt - International Journal of Robust …, 2010 - Wiley Online Library
This paper presents a novel application of backstepping controller for autonomous landing
of a rotary wing UAV (RUAV). This application, which holds good for the full flight envelope …