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Misuzu Haruki
Observed names:
HARUKI, Misuzu,
Haruki, Misuzu,
Misuzu HARUKI
Institution:
Toyota Motor Corporation (Japan)
Observed institutions:
Japan Aerospace Exploration Agency,
Toyota Motor Corporation (Japan)
OpenAlex ID:
A5008735663
Steering Law of Control Moment Gyroscopes for Agile Attitude Maneuvers
2016
·
Takuya Kanzawa
, Misuzu Haruki
, et al.
·
Journal of Guidance Control and Dynamics
·
15
Orbit Plan and Mission Design for Mars EDL and Surface Exploration Technologies Demonstrator
2016
·
Naoko OGAWA
, Misuzu HARUKI
, et al.
·
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES AEROSPACE TECHNOLOGY JAPAN
·
2
PDF
Multidisciplinary Design Method for Off-Road Vehicles Using Bayesian Active Learning
2024
·
Hiroaki Kawamura
, Misuzu Haruki
, et al.
·
SAE technical papers on CD-ROM/SAE technical paper series
GNC Strategy to Capture, Stabilize, and Remove Large Space Debris
2019
·
Toru Yamamoto
, Y. Nakajima
, et al.
·
First International Orbital Debris Conference
Development test of the GNC system for Small Re-entry Capsule Integrated into HTV
2018
·
春木, 美鈴
, 中村, 涼
, et al.
·
Institutional Repositories DataBase (IRDB)
PDF
Active Disturbance Reduction Control with an Adaptive Filter for a Mechanical Cryocooler
2017
·
Shuhei SHIGETO
, Misuzu HARUKI
, et al.
·
The Proceedings of the Dynamics & Design Conference
PDF
Steering Law of Control Moment Gyroscopes for Agile Attitude Maneuvers
2016
·
神澤, 拓也
, 春木, 美鈴
, et al.
·
Institutional Repositories DataBase (IRDB)
PDF
Attitude Maneuver Tests Using CMGs Mounted in a Three-Axis Free Dynamics Simulator
2016
·
Takuya KANZAWA
, Misuzu HARUKI
, et al.
·
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES AEROSPACE TECHNOLOGY JAPAN
PDF
Fault-Tolerant Attitude Control Systems using Multi-Objective Optimization for a Spacecraft Equipped with Control Moment Gyros
2015
·
Ai Noumi
, Masaki Takahashi
, et al.
·
AIAA Guidance, Navigation, and Control Conference and Exhibit
Evaluation of Orbit Determination Accuracy for Mars Landing Demonstrator
2014
·
Takeuchi, Hiroshi
, Ogawa, Naoko
, et al.
·
JAXA Repository (JAXA)
Trajectory Design of Mars Landing Demonstrator
2014
·
Ogawa, Naoko
, Haruki, Misuzu
, et al.
·
JAXA Repository (JAXA)
Development of Pin-Point Landing Technologies for Mars EDL Demonstrator
2014
·
Fujita, Kazuhisa
, Haruki, Misuzu
, et al.
·
JAXA Repository (JAXA)
Trajectory Design of Mars Landing Demonstrator
2014
·
尾川, 順子
, 春木, 美鈴
, et al.
·
Institutional Repositories DataBase (IRDB)
Design of an attitude control system by multi objective optimization considering practical operation of spacecraft equipped with control moment gyros
2014
·
Ai Noumi
, Takuya Kanzawa
, et al.
リスク低減フェーズ#2:spicaの指向擾乱管理に関わる要素技術試作評価結果
2014
·
巳谷, 真司
, 坂井, 真一郎
, et al.
·
Institutional Repositories DataBase (IRDB)
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Works count:
23
Citation count:
18
H-index:
2
I10-index:
1
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