Autonomous Guidance and Control of a Biomimetic Single-wing Mav
نویسندگان
چکیده
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 torque-rod driven trailing-edge flap as the sole control surface. One end is attached to a hub containing a full suite of avionics for measuring its states in all degrees of freedom. While Samarai exhibits the passive rotational stability inherent in maple seeds, the onboard avionics and flight controls give it the added capability of powered flight to specific locations—under high-level operator guidance or autonomously. We will discuss the innovations in vehicle modeling, state sensing/estimation and control needed to realize these capabilities. We will also present experimental results.
منابع مشابه
Modeling and Control of a Dragonfly-like Micro Aerial Vehicle
The purpose of this research is to model and control a dragonflylike flapping wing micro aerial vehicle (FWMAV). It is well known that micro aerial vehicle (MAV) designs can be classified as fixed wing, rotary wing and flapping wing. Fixed wing MAV is capable of fast forward flight, which is suitable for flying outdoor. Rotary wing MAV is suitable for movement at low speed. Recently, flapping w...
متن کاملBounded control of an underactuated biomimetic aerial vehicle - Validation with robustness tests
Flapping wing Micro Aerial Vehicles (FMAVs) have recently emerged as a promising challenge lying on the progress of the avionics technologies. The present paper deals with the development of simple control laws for an embedded implementation on a biomimetic MAV, aiming to control its attitude and position. The control laws are bounded, taking into consideration the amplitude bounds of the contr...
متن کاملDevelopment of c-means Clustering Based Adaptive Fuzzy Controller for A Flapping Wing Micro Air Vehicle
Advanced and accurate modelling of a Flapping Wing Micro Air Vehicle (FW MAV) and its control is one of the recent research topics related to the field of autonomous Unmanned Aerial Vehicles (UAVs). In this work, a four wing Natureinspired (NI) FW MAV is modeled and controlled inspiring by its advanced features like quick flight, vertical take-off and landing, hovering, and fast turn, and enhan...
متن کاملOptic Flow Based Collision Avoidance on a Hybrid MAV
Recent terrorist attacks on the United States have exposed the need for better surveillance and situational awareness technologies. Organizations created to address these needs are aggressively funding research in the use of Micro Air Vehicles for homeland security missions. Such missions have been occurring in caves, tunnels, and urban areas. By mimicking flying insects which navigate in these...
متن کاملNew Concepts and Perspectives on Micro-Rotorcraft and Small Autonomous Rotary-Wing Vehicles
This paper summarizes ongoing work concerning micro-rotorcraft (MRC) – i.e., rotary-wing micro air vehicles (MAV) – research and development. Technology trends involving microelectronic miniaturization, vehicle autonomy systems, electric propulsion and power electronics are contributing to an ongoing revolution in MAV and MRC aerial vehicle concepts and applications. New vehicle configurations ...
متن کامل