# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
1.1 Normal Biological Development And Functioning

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4009 Electronics, Sensors And Digital Hardware

# keywords[]
5102 Atomic, Molecular And Optical Physics

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4007 Control Engineering, Mechatronics And Robotics

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# educationAndTraining[].organization.label
Indian Institute of Technology Bombay - (Mumbai, India)

# educationAndTraining[].organization.label
Indian Institute of Technology Bombay - (Mumbai, India)

# educationAndTraining[].organization.label
University of Maryland, College Park - (College Park, Maryland, United States)

# publications[].label
Flow field studies on a micro-air-vehicle-scale cycloidal rotor in forward flight

# publications[].label
A truly biomimetic hover-capable flapping wing robot

# publications[].label
Performance and flowfield measurements of a meso-scale cycloidal rotor in hover

# publications[].label
Wind Tunnel Studies on a Micro Air VehicleScale Cycloidal Rotor

# publications[].publisher
AHS International dba Vertical Flight Society

# publications[].label
Experimental investigation of a flapping wing concept in hover and forward flight for micro air vehicle applications

# publications[].label
Experimental and Computational Analysis of Rigid Flapping Wings for Micro Air Vehicles

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Design, Development, and Flight Test of a Small-Scale Cyclogyro UAV Utilizing a Novel Cam-Based Passive Blade Pitching Mechanism

# publications[].label
Design and development of an unconventional VTOL micro air vehicle: The Cyclocopter

# publications[].publisher
SPIE, the international society for optics and photonics

# publications[].label
Performance and flowfield measurements of a MAV-scale helicopter rotor in hover

# publications[].label
Experimental and computational investigation of a small-scale vertical axis wind turbine with dynamic blade pitching

# publications[].label
System identification of a robotic hummingbird in hovering flight

# publications[].label
Experimental and computational studies to understand unsteady aerodynamics of cycloidal rotors in hover at ultra-low Reynolds numbers

# publications[].label
Performance Measurements of Meso-Scale Cyclodial Rotors in Hover

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Nonlinear aeroelastic coupled trim analysis of FlappingWing MAV in hover

# publications[].label
Control of a biomimetic flapping mechanism for a hovering micro air vehicle

# publications[].label
Improving the Aerodynamic Performance of Micro-Air-Vehicle-Scale Cycloidal Rotor: An Experimental Approach

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Development of a meso-scale cycloidal-rotor aircraft for micro air vehicle application

# publications[].label
Design, Development, and Open-Loop Flight-Testing of a Twin-Rotor Cyclocopter Micro Air Vehicle

# publications[].publisher
AHS International dba Vertical Flight Society

# publications[].label
Development of a Quad Cycloidal-Rotor Unmanned Aerial Vehicle

# publications[].publisher
AHS International dba Vertical Flight Society

# publications[].label
Hydrodynamic modeling and experimental validation of a cycloidal propeller

# publications[].label
Aeroacoustic analysis of UAV-scale cycloidal rotor: An experimental and computational approach

# publications[].label
Flight dynamics identification of a cyclocopter micro air vehicle in hover

# publications[].label
Design and development of a hover-capable flapping wing micro air vehicle

# publications[].label
Development of a 100-gram micro-cyclocopter capable of autonomous hover

# publications[].label
Towards a fundamental understanding of low reynolds number flapping wing aerodynamics

# publications[].label
On the development of a robotic hummingbird

# publications[].label
Aeroelastic analysis of a MAV-Scale cycloidal rotor

# publications[].label
Experimental Studies on a Mesoscale Cycloidal Rotor in Hover

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Hover Performance of a Small-Scale Helicopter Rotor for Flying on Mars

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Performance of a Cycloidal Rotor Concept for Micro Air Vehicle Applications

# publications[].publisher
AHS International dba Vertical Flight Society

# publications[].label
Effect of Rotor Geometry and Blade Kinematics on Cycloidal Rotor Hover Performance

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Performance measurements of UAV-scale cycloidal rotor

# publications[].label
Aerodynamics of a Small-Scale Vertical-Axis Wind Turbine with Dynamic Blade Pitching

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Flight dynamics identification, maneuverability, and gust tolerance of a robotic hummingbird in hover

# publications[].label
Experimental investigation of a flapping wing concept in hover and forward flight for micro air vehicle applications

# publications[].label
Understanding insect-based flapping flight from a micro air vehicle perspective

# publications[].label
Experimental Studies to Understand the Hover and Forward Flight Performance of a MAV-Scale Flapping Wing Concept

# publications[].publisher
AHS International dba Vertical Flight Society

# publications[].label
Force and Flowfield Measurements on a Rigid Wing Undergoing Hover-Capable Flapping and Pitching Kinematics in Air at MAV-Scale Reynolds Numbers

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Effect of Flow Curvature on Forward Flight Performance of a Micro-Air-Vehicle-Scale Cycloidal-Rotor

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
System identification of a meso-scale twin-cyclocopter in hover

# publications[].label
Experimental studies towards understanding the aeromechanics of a flexible robotic hummingbird wing in hover

# publications[].label
Nonlinear aeroelastic model for a highly flexible flapping wing in hover

# publications[].label
Experimental optimization of UAV-Scale cycloidal rotor performance

# publications[].label
CFD-CSD coupled aeroelastic analysis of a highly flexible flapping wing in hover

# publications[].label
A novel mechanism for emulating insect wing kinematics.

# publications[].label
Force and flowfield measurements to understand unsteady aerodynamics of cycloidal rotors in hover at ultra-low Reynolds numbers

# publications[].label
Design and development of a Meso-Scale Cyclocopter

# publications[].label
Design and hover testing of a 60-gram cyclocopter

# publications[].label
Understanding Micro Air Vehicle Flapping-Wing Aerodynamics Using Force and Flowfield Measurements

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Force and Flowfield Measurements on a Rigid Wing Undergoing Hover-Capable Flapping and Pitching Kinematics in Air at MAV-Scale Reynolds Numbers

# publications[].publisher
American Institute of Aeronautics and Astronautics

# publications[].label
Development of Control Strategies for a Twin-Cyclocopter in Forward Flight

# publications[].publisher
AHS International dba Vertical Flight Society

# publications[].label
Aerodynamic Simulation of High-Speed Capsule in the Hyperloop System

# publications[].publisher
American Institute of Aeronautics and Astronautics

# publications[].label
Development and Flight Testing of a Meso-Scale Cyclopter

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Aeroelastic analysis for highly flexible flappingwing in hover

# publications[].label
Experimental Optimization of MAVScale Cycloidal Rotor Performance

# publications[].publisher
AHS International dba Vertical Flight Society

# publications[].label
Design and development of a hover-capable cyclocopter micro air vehicle

# publications[].label
Development of a Robotic Hummingbird Capable of Controlled Hover

# publications[].publisher
AHS International dba Vertical Flight Society

# publications[].label
Cycloidal Rotor-Blade Tip-Vortex Analysis at Low Reynolds Number

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Experiments on Rigid Wing Undergoing Hover-Capable Flapping Kinematics at Micro-Air-Vehicle-Scale Reynolds Numbers

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Understanding Unsteady Aerodynamics of Cycloidal Rotors in Hover at Ultra-low Reynolds Numbers

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Performance of a small-scale helicopter rotor for martian applications

# publications[].label
Aerodynamic Simulation of High-Speed Capsule in the Hyperloop System

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Experimental and computational flow field studies of a MAV-scale cycloidal rotor in forward flight

# publications[].label
Semi-empirical modeling of group 1 UAS electric powertrains

# publications[].label
Towards a fundamental understanding of low reynolds number flapping wing aerodynamics

# publications[].label
Effects of Asymmetric Blade-Pitching Kinematics on Forward-Flight Performance of a Micro-Air-Vehicle-Scale Cycloidal-Rotor

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Effect of rotor geometry on UAV-scale cycloidal rotor hover performance

# publications[].label
Development of a gun-launched rotary-wing micro air vehicle

# publications[].label
Aeroelastic Analysis of a Micro-Air-Vehicle-Scale Cycloidal Rotor in Hover

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Experimental and computational aerodynamic investigation of avian-based rigid flapping wings for MAV applications

# publications[].label
Tip vortex measurements on a cycloidal rotor blade at ultralow Reynolds numbers

# publications[].label
Experimental performance optimization of a MAV-scale cycloidal rotor

# publications[].label
Flight dynamics modeling and system identification of a cyclocopter in forward flight

# publications[].label
Design and Development of a 30 g Cyclocopter

# publications[].publisher
AHS International dba Vertical Flight Society

# publications[].label
Role of Blade Flexibility on Cycloidal Rotor Hover Performance

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Experimental investigation of the forward flight performance of a MAV-scale cycloidal rotor

# publications[].label
Fundamental Understanding of the Physics of a Small-Scale Vertical Axis Wind Turbine with Dynamic Blade Pitching: An Experimental and Computational Approach

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Symmetric Versus Asymmetric Pitching of a Cycloidal Rotor Blade at Ultra-Low Reynolds Numbers

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Gust disturbance rejection study of a cyclocopter micro air vehicle

# publications[].label
Development of a cantilevered rotor-based meso-cyclocopter

# publications[].label
Identification of Flight Dynamics of a Cylcocopter Micro Air Vehicle in Hover

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Nonlinear aeroelastic modeling of cycloidal rotor in forward flight

# publications[].label
Coupled CFD/CSD-based aeroelastic analysis with flowfield measurements of avian-based flexible flapping wings for MAV applications

# publications[].label
Experimental investigation of the effect of rotor geometry and blade kinematics on the performance of a MAV-scale cycloidal rotor

# publications[].label
Design, development and flight testing of a twin-rotor cyclocopter micro air vehicle

# publications[].label
Design, development, and flight testing of a high endurance micro quadrotor helicopter

# publications[].label
Fundamental Understanding of the Physics of a Small-Scale Vertical Axis Wind Turbine with Dynamic Blade Pitching: An Experimental and Computational Approach

# publications[].publisher
American Institute of Aeronautics and Astronautics

# publications[].label
Autonomous hover capability of cycloidal-rotor Micro Air Vehicle

# publications[].label
Understanding effect of blade flexibility on cycloidal rotor hover performance

# publications[].label
Experimental and computational studies to understand the role of flow curvature effects on the aerodynamic performance of a MAV-scale cycloidal rotor in forward flight

# publications[].label
Design, development, and flight testing of a high endurance micro quadrotor helicopter

# publications[].label
Aeromechanics Analysis of a Hummingbird-Like Flapping Wing in Hover

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Experiments on the optimization of MAV-scale cycloidal rotor characteristics towards improving their aerodynamic performance

# publications[].label
Aeroelastic Analysis of Avian-Based Flexible Flapping Wings for Micro Air Vehicles

# publications[].publisher
AHS International dba Vertical Flight Society

# publications[].label
Nonlinear aeroelastic coupled trim analysis of a cyclocopter in hover

# publications[].label
Experimental investigation of an insect-based flapping wing hovering micro air vehicle

# publications[].label
Development of a Micro Twin-Rotor Cyclocopter Capable of Autonomous Hover

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
A Deep Reinforcement Learning Control Strategy for Vision-based Ship Landing of Vertical Flight Aircraft

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Experimental Investigation of Micro Air Vehicle Scale Helicopter Rotor in Hover

# publications[].label
Experimental investigation of the cycloidal-rotor concept for a hovering micro air vehicle

# publications[].label
Development of a 200 gram twin-rotor micro cyclocopter capable of autonomous hover

# publications[].label
Experimental and computational studies to understand the role of flow curvature effects on the aerodynamic performance of a MAV-scale cycloidal rotor in forward flight

# publications[].label
Nonlinear aeroelastic coupled trim analysis of a twin-cyclocopter in forward flight

# publications[].label
Development of control strategies and flight testing of a twin-cyclocopter in forward flight

# publications[].label
CFD analysis for flexible flapping wing in hover flight

# publications[].label
Design, development and flight-testing of a robotic hummingbird

# publications[].label
Development of the world's smallest cyclocopter

# researcherOn[].label
Instrumentation for Performance, Blade Loads and Flowfield Measurement of Novel Hover-Capable Meso-Scale Aerial Platforms

# researcherOn[].awardedBy.label
United States Army - (Washington D.C., District of Columbia, United States)

# researcherOn[].label
Dynamics and Control of Hummingbird Inspired Aerial Robots

# researcherOn[].awardedBy.label
National Science Foundation - (Arlington, Virginia, United States)

# researcherOn[].label
Topic Area 3.H: Model-Based Engineering for Design Space Exploration of VTOL UASs

# researcherOn[].awardedBy.label
United States Army - (Washington D.C., District of Columbia, United States)

# researcherOn[].label
A Novel Amphibious Platform with Stowable Cycloidal Propellers

# researcherOn[].awardedBy.label
United States Department of the Navy - (Arlington, Virginia, United States)

# researcherOn[].label
Topic Area 3. C: Aeromechanics, Flight Dynamics and Control of a Revolutionary Tube-Launched Rotorcraft

# researcherOn[].awardedBy.label
United States Army - (Washington D.C., District of Columbia, United States)

# researcherOn[].label
Phase II IUCRC Texas A&M University: Center for Unmanned Air Systems C-UAS

# researcherOn[].awardedBy.label
Directorate for Computer & Information Science & Engineering - (Arlington, Virginia, United States)

# streetAddress
Texas A&M University; Aerospace Engineering; 3141 TAMU