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Retricted access

Research article

First published 2017-3

Vibration reduction of helicopter with trailing-edge flaps at various flying conditions

SK Kodakkattu, ML Joy, K Prabhakaran Nair

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 1983-8-1

The autogyro for ship propulsion

N. Bose

International Shipbuilding Progress

Open access

Research article

First published 2015-10

Enhanced Hover Control of Quad Tilt Frame UAV under Windy Conditions

R. Krishnakumar, A. Mohamed Rasheed, K. Senthil Kumar

International Journal of Advanced Robotic Systems

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Research article

First published 2023-3

Self-tuning control of parametrically excited active magnetic bearing system due to harmonic base motion using fuzzy logic

Tukesh Soni, Jayanta K Dutt, AS Das

Journal of Vibration and Control

Retricted access

Research article

First published 2004-12

Theory and practice: Requirements for adhesive bonding in marine structures

G Wacker, D Brügge, K Fach [...]

Proceedings of the Institution of Mechanical Engineers,Part M: Journal of Engineering for the Maritime Environment

Free access

Research article

First published 2009-12

Optical Flow for Heading Estimation of a Quadrotor Helicopter

John Stowers, Andrew Bainbridge-Smith, Michael Hayes [...]

International Journal of Micro Air Vehicles

Open access

Research article

First published 2015-7

Experimental Investigation for RUAV's Actuator Fault Detections with AESMF

Dalei Song, Juntong Qi, Liying Yang [...]

International Journal of Advanced Robotic Systems

Search results

Vibration reduction of helicopter with trailing-edge flaps at various flying conditions

The autogyro for ship propulsion

Enhanced Hover Control of Quad Tilt Frame UAV under Windy Conditions

Self-tuning control of parametrically excited active magnetic bearing system due to harmonic base motion using fuzzy logic

Theory and practice: Requirements for adhesive bonding in marine structures

Optical Flow for Heading Estimation of a Quadrotor Helicopter

Experimental Investigation for RUAV's Actuator Fault Detections with AESMF