CDMA functional blocks using recycling integrator correlators-matched filters and delay-locked loops. - Kunihiko Iizuka; Masayuki Miyamoto; Yoshiji Ohta; Takahiro Suyama; Keita Hara; Shuichi Kawama; Hirofumi Matsui; Shin'ichiro Azuma; Shigenari Taguchi; Yoshihisa Fujimoto; Daniel Senderowicz (IEEE J. Solid State Circuits, 2001)

Free-flight Analysis of Flapping Flight during Turning by Fluid-structure Interaction Finite Element Analysis based on Arbitrary Lagrangian-Eulerian Method. - Masaki Hamamoto; Yoshiji Ohta; Keita Hara; Toshiaki Hisada (ICRA, 2004)

Design of Flexible Wing for Flapping Flight by Fluid-Structure Interaction Analysis. - Masaki Hamamoto; Yoshiji Ohta; Keita Hara; Toshiaki Hisada (ICRA, 2005)

Feasibility Study of an Actuator for Flapping Flight using Fluid-structure Interaction Analysis. - Masaki Hamamoto; Yoshiji Ohta; Keita Hara; Toshiaki Hisada (ICRA, 2006)

Application of fluid-structure interaction analysis to flapping flight of insects with deformable wings. - Masaki Hamamoto; Yoshiji Ohta; Keita Hara; Toshiaki Hisada (Adv. Robotics, 2007)

Basic Design Strategy for Stiffness Distribution on a Dragonfly-Mimicking Wing for a Flapping Micro Aerial Vehicle. - Masaki Hamamoto; Yoshiji Ohta; Keita Hara; Toshiaki Hisada (Adv. Robotics, 2010)

A Fundamental Study of Wing Actuation for a 6-in-Wingspan Flapping Microaerial Vehicle. - Masaki Hamamoto; Yoshiji Ohta; Keita Hara; Toshiaki Hisada (IEEE Trans. Robotics, 2010)

Free-flight analysis of dragonfly hovering by fluid-structure interaction analysis based on an arbitrary Lagrangian-Eulerian method. - Masaki Hamamoto; Yoshiji Ohta; Keita Hara; Toshiaki Hisada (Adv. Robotics, 2013)

Investigation on force transmission of direct-drive thorax unit with four ultrasonic motors for a flapping microaerial vehicle. - Masaki Hamamoto; Teruhisa Kotani; Ikuo Nakano; Yoshiji Ohta; Keita Hara; Yoshiteru Murakami; Toshiaki Hisada (Adv. Robotics, 2014)