By Kimon P. Valavanis
There was great emphasis in unmanned aerial autos, either one of mounted (airplanes) and rotary wing (vertical take off and touchdown, helicopters) varieties during the last ten years. purposes span either civilian and armed forces domain names, the latter being an important at this level. This edited e-book presents a great and varied reference resource regarding uncomplicated, utilized study and improvement on small and miniature unmanned aerial autos, either fastened and rotary wing. As such, the booklet deals history info at the evolution of such autos through the years, through modeling and keep watch over basics which are of paramount value because of unmanned aerial motor vehicle version complexity, nonlinearity, coupling, inhirent instability and parameter values uncertainty. points of navigation, together with visual-based navigation and objective monitoring are mentioned, through purposes to perspective estimation on micro unmanned aerial automobiles, independent sun unmanned aerial car, biomimetic sensing for independent flights in near-earth environments, localization of air-ground instant sensor networks, decentralized formation monitoring, layout of an unmanned aerial motor vehicle for volcanic gasoline sampling and layout of an on-board processing controller for miniature helicopters.
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Additional resources for Advances in Unmanned Aerial Vehicles: State of the Art and the Road to Autonomy (Intelligent Systems, Control and Automation: Science and Engineering)
P. Valavanis ¾ Chapter 6 takes advantage of progress in low-power processors and miniature sensors to design and control a miniature quadrotor. This is a rather difficult problem in the field of miniature flying robots (MFR) that are used in search and rescue missions, after earthquakes, explosions, collapsed buildings, etc, since such a MFR should fit through small openings, maneuver around pillars and destructed wall structures. x Part III is devoted to autonomous navigation, discussing approaches that contribute to improving UAV autonomicity, a key requirement dictated by the US DOD  .
It is designed as a reusable, low cost alternative to cruise missiles . Fig. 39. The Eagle Eye by Bell Textron. The tilt-rotor configuration is to be evaluated in 2007 . Fig. 40. The Neptune built by DRS Unmanned Technologies. Surveillance vehicle designed for sea-launch and recovery from small vessels . 36 K. P. Valavanis, M. Kontitsis Fig. 41. The Maverick built by Boeing/Frontier/Robinson utilized as a testbed for development of control logic . Fig. 42. The XPV-1 built by BAI Aerosystems.
By exploiting the natural geometry of the group of rotations an attitude observer is derived that: requires only accelerometer and gyro outputs; it is suitable for implementation on embedded hardware, and, provides robust attitude estimates as well as estimating the gyro biases on-line. ¾ Chapter 12 refers to autonomous solar UAV for sustainable flights. A methodology is presented that is suitable for the global design of a solar powered airplane intended to achieve continuous flight on Earth. ¾ Chapter 13 illustrates how integrating optic flow sensing for lateral collision avoidance with a novel MAV platform results in a vehicle that is well suited for flight in near-Earth environments.