Aeromechanical Design and Analysis of H-Drone Configuration-Reference-Cited by-同舟云学术

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Aeromechanical Design and Analysis of H-Drone Configuration

Published:2022-05-04 Issue: Volume: Page:
ISSN:
Container-title:2022 13th Asian Control Conference (ASCC)
language:
Short-container-title:

Author:

Dwarakanathan D¹,Raja S¹,Shanmugam P²,Shashank D³,Rohan M⁴,Selvam C⁵,Kevin R Sanjeeth⁵,Katta Sree S S⁶,Saha S K⁶

Affiliation:

1. CSIR-National Aerospace Laboratories,Structural Technological Division,Bangalore,India

2. CSIR-National Aerospace Laboratories,Unmanned Aerial Vehicle Division,Bangalore,India

3. Indian Institute of Technology Delhi,I - Hub Foundation for Cobotics,New Delhi,India

4. MIT - WP University Pune,School of Mechanical Engineering,Maharashtra,India

5. Blue Hat Solutions Private Limited,Bangalore,India

6. Indian Institute of Technology Delhi,Dept. of Mechanical Engineering,New Delhi,India

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9828005/9828007/09828119.pdf?arnumber=9828119

Reference10 articles.

1. Aerodynamic Performance of Quadrotor UAV with Non-Planar Rotors

2. ADAPTIVE SLIDING MODE CONTROL OF UNMANNED FOUR ROTOR FLYING VEHICLE

3. Force Simulation Analysis of Underground Quadrotor UAV Based on Virtual Laboratory Technology

4. Disturbance observer based hierarchical control of coaxial-rotor UAV

5. The Stability Analysis of Quadrotor Unmanned Aerial Vechicles

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