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Autonomous Control Systems and Vehicles

Part of the Intelligent Systems, Control and Automation: Science and Engineering Book Series (volume 65)

Editors: Nonami, Kenzo; Kartidjo, Muljowidodo; Yoon, Kwang-Joon; Budiyono, Agus

DOI: 10.1007/978-4-431-54276-6

ISBN: 978-4-431-54275-9

Publisher: Springer Japan - Springer Journals

Mar 16, 2013

1 - 10 of 21 Chapters

Available

Flight Demonstrations of Fault Tolerant Flight Control Using Small UAVs

Suzuki, Shinji; Yoshimatsu, Yuka; Miyaji, Koichi

Pages: 3 –19

[Fault tolerant flight control (FTFC) has been investigated to increase aviation safety. FTFC adaptively changes control devices, control algorithms, or control parameters in order to regulate the change of dynamic characteristics of aircraft when malfunction of control system or airframe...
Available

Unmanned Aerial and Ground Vehicle Teams: Recent Work and Open Problems

Waslander, Steven L.

Pages: 21 –36

[Unmanned aerial and ground vehicle teams present a majoropportunity for expanded operation over individual autonomous vehicles alone. The different perspectives available for sensors, the different operating ranges and payload capabilities, and the ability to observe a target environment from...
Available

Cognitive Developmental Robotics: from Physical Interaction to Social One

Asada, Minoru

Pages: 37 –51

[Cognitive Developmental Robotics (CDR) aims to provide new understanding how human’s higher cognitive functions develop by means of a synthetic approach that developmentally constructs cognitive functions. The key idea of CDR is “from physical embodiment to social interaction” that enables...
Available

Towards a Unified Framework for UAS Autonomy and Technology Readiness Assessment (ATRA)

Kendoul, Farid

Pages: 55 –71

[As the number of programs for developing autonomous unmanned aircraft systems (UAS) accelerates, there is a growing need for a comprehensive framework that allows UAS practitioners, particularly researchers, to characterize, compare, and assess the UAS autonomy technologies from the perspectives...
Available

Control Scheme for Automatic Takeoff and Landing of Small Electric Helicopter

Suzuki, Satoshi

Pages: 73 –83

[In this study, a control scheme and controller design for automatic takeoff and landing of a small unmanned helicopter are proposed. First, acceleration feedback controller is designed for stabilizing horizontal motion of the helicopter. In acceleration feedback controller, horizontal...
Available

Evaluation of an Easy Operation System for Unmanned Helicopter

Miwa, Masafumi; Nakamatsu, Shouta; Kinoshita, Kentaro

Pages: 85 –95

[In this study, we present an easy operation system for unmanned helicopter. The aim of this system is simplification of the control operation and safety improvement for beginner’s flight and aerial photographing. This system consists of R/C helicopter, attitude/position control system, and a...
Available

Control of Ducted Fan Flying Object Using Thrust Vectoring

Miwa, Masafumi; Shigematsu, Yuki; Yamashita, Takashi

Pages: 97 –107

[Recently, R/C helicopter is used in fields of aerial photography and aerial investigation. But helicopter rotor blades are not covered, and the thrust is generated by high rotational speed. Thus R/C helicopter has a high risk of damage. In this study, we developed a new flying object using...
Available

Circular Formation Control of Multiple Quadrotor Aerial Vehicles

Abas, M. Fadhil; Pebrianti, Dwi; Azrad, Syaril; Iwakura, D.; Song, Yuze; Nonami, K.

Pages: 109 –132

[This chapter describes the circular leader–follower formation control for multiple quadrotor aerial vehicles (QAVs). The strategy used in this chapter is to apply the control algorithm for conducting a circular motion. This task is known to be important since a trajectory is a combination of...
Available

Decentralised Formation Control of Unmanned Aerial Vehicles Using Virtual Leaders

Hino, Takuma; Tsuchiya, Takeshi

Pages: 133 –144

[In this chapter, a simple but robust formation control scheme for unmanned aerial vehicles is proposed. The proposed scheme is based on the virtual leader approach. Mathematical proof is provided to show that the scheme allows formations to converge, as long as sufficient communications between...
Available

Aerodynamics and Flight Stability of Bio-inspired, Flapping-Wing Micro Air Vehicles

Liu, Hao; Wang, Xiaolan; Nakata, Toshiyuki; Yoshida, Kazuyuki

Pages: 145 –157

[In this chapter, we present an integrated study of flexible wing aerodynamics and passive dynamic flight stability of a prototype bio-inspired, flapping-wing micro air vehicle (MAV) by a combination of flexible wing kinematics and force measurements and computational approaches. The MAV is...

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