منابع مشابه
Targeted Autonomous Indoor Flight of a Rotary-Wing MAV
The paper is focused on the development of algorithms for Autonomous Rotary-Wing Micro Aerial Vehicles (RW MAVs) in indoor GPS-denied environments. In such missions, GPS may be unavailable and the map of the environment is a priory unknown. This paper presents a modular system consisted of the required components for flying RW MAVs in indoor environments. These components include the methods fo...
متن کاملAutonomous Guidance and Control of a Biomimetic Single-wing Mav
We discuss the guidance and control of the Samarai MAV—a single-winged, wholly rotating, biomimetic micro air vehicle developed at Lockheed Martin Advanced Technology Laboratories. Samarai is inspired by, and named after, the samara or maple seed Acer diabolicum Blume. It weighs 200 grams and consists of a single wing of radius 30 centimeters with an electric motor/propeller at the tip and torq...
متن کاملImproving flight performance of the flapping wing MAV DelFly II
Recent years have seen an increasing interest in micro aerial vehicles (MAVs) and flapping flight in connection to that. The Delft University of Technology has developed a flapping wing MAV, “DelFly II”, which relies on a flapping bi-plane wing configuration for thrust and lift. The ultimate aim of the present research is to improve the flight performance of the DelFly II from both an aerodynam...
متن کاملstudy of wing shapes influence on mav aerodynamic coefficients
in recent years, design of small aircrafts are studied and extensively developed. one of the most important of these aircrafts is micro aerial vehicles (mavs). as part of aerodynamic design of mavs, the wing design is important. in fact, the main part of this design is to find an appropriate shape for the wing. in this work, influence of the wing shape at low reynolds number flow is investigate...
متن کاملModel Update of a Micro Air Vehicle (MAV) Flexible Wing Frame with Uncertainty Quantification
This paper describes a procedure to update parameters in the finite element model of a Micro Air Vehicle (MAV) to improve displacement predictions under aerodynamics loads. Because of fabrication, materials, and geometric uncertainties, a statistical approach combined with Multidisciplinary Design Optimization (MDO) is used to modify key model parameters. Static test data collected using photog...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
ژورنال
عنوان ژورنال: Theoretical and Applied Mechanics Letters
سال: 2013
ISSN: 2095-0349
DOI: 10.1063/2.1306202