Integrated electro-aeromechanical structures for low-cost, self-deploying environment sensors and disposable UAVs

@article{Pounds2013IntegratedES,
  title={Integrated electro-aeromechanical structures for low-cost, self-deploying environment sensors and disposable UAVs},
  author={Paul E. I. Pounds and Surya P. N. Singh},
  journal={2013 IEEE International Conference on Robotics and Automation},
  year={2013},
  pages={4459-4466}
}
This paper presents a novel approach for constructing light-weight, low-cost air-deployable sensor modules and miniature unmanned aerial vehicles which consist of printed circuit boards as integrated electronic, structural and aerodynamic lift-producing devices. In this way, each aircraft can be a single-piece, single-manufacturing step assembly, reducing materials, processing and labour costs. This approach allows the fabrication of devices that are sufficiently inexpensive so as to be… 

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References

SHOWING 1-10 OF 39 REFERENCES

Paper Plane: Towards Disposable Low-Cost Folded Cellulose-Substrate UAVs

Disposable folded cellulose-substrate micro-Unmanned Aerial Vehicles (UAVs) - paper planes - have the surprising potential to be effective platforms for deploying remote sensors at low-cost. With

Small-scale Aeroelastic Rotor Simulation, Design and Fabrication

Efficient, small-scale fixed-pitch rotor blades are essential for miniature rotorcraft. Extremely thin blade sections are required for highly efficient rotor performance that leads to acceptable

RoACH: An autonomous 2.4g crawling hexapod robot

TLDR
This work presents the design, fabrication, and testing of a novel hexapedal walking millirobot using only two actuators, which is the smallest and lightest autonomous legged robot produced to date.

Design of a Static Thruster for Microair Vehicle Rotorcraft

This paper presents a case study of a design for a complete microair vehicle thruster. Fixed-pitch small-scale rotors, brushless motors, lithium-polymer cells, and embedded control are combined to

Microrobot Design Using Fiber Reinforced Composites

Mobile microrobots with characteristic dimensions on the order of 1 cm are difficult to design using either microelectromechanical systems technology or precision machining. This is due to the

Autonomous Flight of a Samara MAV

TLDR
Advantages over traditional micro-scaled VTOL configurations include passive stability, efficient autorotation, low body drag, mechanical simplicity, low cost, high payload capacity, and substantial damage tolerance.

From falling to flying: the path to powered flight of a robotic samara nano air vehicle

TLDR
Inspired by the flight modalities of the bio-inspired samaras, a robotic device has been created that mimics the autorotative capability of the samara, whilst providing the ability to hover, climb and translate.

Bio-inspired design and dynamic maneuverability of a minimally actuated six-legged robot

Rapidly running arthropods like cockroaches make use of passive dynamics to achieve remarkable locomotion performance with regard to stability, speed, and maneuverability. In this work, we take

On the aerodynamics of paper airplanes

The design of Micro Air Vehicles (MAV) is challenging since the aerodynamic efficiency of airfoils and wings decreases at low Reynolds-numbers. While many MAV approaches investigate biological

First controlled vertical flight of a biologically inspired microrobot

TLDR
Experimental results on altitude control of a flying microrobot using a static flapping experimental setup and the design of the proposed controller relies on the idea of treating an exciting signal as a subsystem of the micRORobot.