Towards Bio-Inspired Robotic Aircraft: Control Experiments on Flapping and Gliding Flight
نویسندگان
چکیده
THERE is a growing interest in the aerospace community in the development of robotic micro aerial vehicles (MAVs) to learn and mimic avian flight. MAVs fly in low-Reynolds-number regimes of 10 to 10, which corresponds to that of small birds or bats [1]. MAVs with wings equipped with multiple degrees of freedom such as flapping, wing twist, and sweep provide greater payload capability than insect-like MAVs and greater maneuverability than conventional fixed-wing aircraft. These MAVs can be used for intelligence gathering, surveillence, and reconnaissance missions in tightly constrained spaces such as forests and urban areas. Advances in actuators and control systems have led to development and analysis of articulated and flapping MAVs inspired by animals [2–5]. Birds and bats achieve remarkable stability and perform agile manuevers using their wings very effectively [2]. One of the goals of reverse-engineering animal flight is to learn more about the various aspects of avian flight such as stability, maneuverability, and control from the dynamics of MAV. From a controls standpoint, there are three major flight regimes or modes in animals: high-frequency flapping, low-frequency flapping, and gliding. Insects reside almost entirely in the high-frequency domain, utilizing small musculature to produce passive pitching dynamics over the course of several wingbeats [6]. For these situations, we can utilize averaging theorems to greatly aid control design around trim states such as hover condition [3, 7, 8]. Much bat and bird flight is low frequency enough that averaging theorems do not apply in practice and intrawingbeat effects are significant [9]. Additionally, steady-state equilibria (or approximations thereof) do not exist, which distinguishes this regime from the other two. Dietl and Leonard give examples of an analysis of this regime by
منابع مشابه
Towards Bio-inspired Robotic Aircraft: CPG-based Control of Flapping and Gliding Flight
This paper presents experimental micro aerial vehicle (MAV) research with low-frequency flapping and articulated wing gliding. The importance of phase difference control via an abstract mathematical model of central pattern generators (CPGs) is confirmed with a robotic bat on a 3-DOF pendulum platform. An aerodynamic model for the robotic bat based on the complex wing kinematics is presented. C...
متن کاملA Flight Mechanics-Centric Review of Bird-Scale Flapping Flight
This paper reviews the flight mechanics and control of birds and bird-size aircraft. It is intended to fill a niche in the current survey literature which focuses primarily on the aerodynamics, flight dynamics and control of insect scale flight. We review the flight mechanics from first principles and summarize some recent results on the stability and control of birds and bird-scale aircraft. B...
متن کاملModeling Synchronous Muscle Function in Insect Flight: a Bio-Inspired Approach to Force Control in Flapping-Wing MAVs
Micro-aerial vehicles (MAV) and their promising applications—such as undetected surveillance or exploration of environments with little space for land-based maneuvers—are a wellknown topic in the field of aerial robotics. Inspired by high maneuverability and agile flight of insects, over the past two decades a significant amount of effort has been dedicated to research on flappingwing MAVs, mos...
متن کاملNeuroinspired Control Strategies with Applications to Flapping Flight
This dissertation is centered on a theoretical, simulation, and experimental study of control strategies which are inspired by biological systems. Biological systems, along with sufficiently complicated engineered systems, often have many interacting degrees of freedom and need to excite large-displacement oscillations in order to locomote. Combining these factors can make high-level control de...
متن کاملEfficiency of Lift Production in Flapping and Gliding Flight of Swifts
Many flying animals use both flapping and gliding flight as part of their routine behaviour. These two kinematic patterns impose conflicting requirements on wing design for aerodynamic efficiency and, in the absence of extreme morphing, wings cannot be optimised for both flight modes. In gliding flight, the wing experiences uniform incident flow and the optimal shape is a high aspect ratio wing...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
عنوان ژورنال:
دوره شماره
صفحات -
تاریخ انتشار 2012