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Orientation filter and angular rates estimation in monocopter using accelerometers and magnetometer with the Extended Kalman Filter.

, , , , and . ICRA, page 4537-4543. IEEE, (2017)

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Optimized Transition Path of a Transformable HOvering Rotorcraft (THOR)., , , , , and . AIM, page 460-465. IEEE, (2018)Direction Controlled Descent of Samara Autorotating Wings (SAW) with N-Wings * Research supported by the SUTD-MIT International Design Centre (IDC) and by the Temasek Laboratories Defence Innovation Research Programme (DIRP) IGDSP15020141., , , , , , and . ICRA, page 6553-6559. IEEE, (2018)Orientation filter and angular rates estimation in monocopter using accelerometers and magnetometer with the Extended Kalman Filter., , , , and . ICRA, page 4537-4543. IEEE, (2017)Design and dynamic analysis of a Transformable Hovering Rotorcraft (THOR)., , , , , and . ICRA, page 6389-6396. IEEE, (2017)Design of a Hybrid Aerial Robot with Multi-Mode Structural Efficiency and Optimized Mid-Air Transition., , , , and . Unmanned Syst., 7 (4): 195-213 (2019)Analysis of wing twist effects on hover flight dynamics of a single rotor aerial craft., , and . AIM, page 323-328. IEEE, (2016)The effects of chordwise wing optimization of single-winged samara in autorotation., , , , , and . AIM, page 815-820. IEEE, (2017)Towards a Stable Three-Mode Transformable HOvering Rotorcraft (THOR)., , , , and . AIM, page 492-497. IEEE, (2018)