Kenshiro (Ken) Oguri
Title
Cited by
Cited by
Year
EQUULEUS mission analysis: Design of the science orbit phase
K Oguri, K Kakihara, S Campagnola, N Ozaki, K Oshima, T Yamaguchi, ...
26th International Symposium on Space Flight Dynamics, 1-7, 2017
112017
Mission to Earth-Moon Lagrange Point by a 6U CubeSat: EQUULEUS
R Funase, N Ozaki, S Nakajima, K Oguri, K Miyoshi, S Campagnola, ...
8th Nano-Satellite Symposium,(Ehime, Japan), 2017
102017
Mission Analysis for EQUULEUS, JAXA’s Earth-Moon Libration Orbit Cubesat
S Campagnola, N Ozaki, K Oguri, Q Verspieren, K Kakihara, K Yanagida, ...
67th International Astronautical Congress, 2016
82016
Mission Analysis for EQUULEUS and OMOTENASHI
S Campagnola, N Ozaki, J Hernando-Ayuso, K Oshima, T Yamaguchi, ...
31th International Symposium on Space Technology and Science, Ehime, Japan, 2017
72017
EQUULEUS mission analysis: Design of the transfer phase
K Oshima, S Campagnola, CH Yam, Y Kayama, Y Kawakatsu, N Ozaki, ...
International Symposium on Space Technology and Science, ISTS-2017-d-159 …, 2017
62017
Mission analysis for the EM-1 CubeSats EQUULEUS and OMOTENASHI
S Campagnola, J Hernando-Ayuso, K Kakihara, Y Kawabata, ...
IEEE AES Mag. 34 (4), 38-44, 2019
42019
Convex Optimization over Sequential Linear Feedback Policies with Continuous-time Chance Constraints
K Oguri, M Ono, JW McMahon
2019 IEEE 58th Conference on Decision and Control (CDC), 6325-6331, 2019
32019
SRP-based orbit control with application to small body landing
K Oguri, JW McMahon
AAS/AIAA Astrodynamics Specialist Conference, 1-19, 2018
32018
Design Criteria of Reflectivity Control System Under Uncertainty in Sail Property for Maneuverability Requirement of Spinning Solar Sail
K Oguri, T Kudo, R Funase
AIAA/AAS Astrodynamics Specialist Conference, 5674, 2016
32016
Area-of-Effect Softbots (AoES) for Asteroid Proximity Operations
J McMahon, SK Mitchell, K Oguri, N Kellaris, D Kuettel, C Keplinger, ...
2019 IEEE Aerospace Conference, 1-16, 2019
22019
Risk-aware Trajectory Design with Continuous Thrust: Primer Vector Theory Approach
K Oguri, JW McMahon
AAS/AIAA Astrodynamics Specialist Conference, Portland, ME, 2019
22019
Risk-aware Trajectory Design with Impulsive Maneuvers: Convex Optimization Approach
K Oguri, JW McMahon
AAS/AIAA Astrodynamics Specialist Conference, Portland, ME, 2019
22019
Attitude Determination and Control System for the PROCYON Micro-Spacecraft
S Ikari, T Inamori, T Ito, K Ariu, K Oguri, M Fujimoto, S Sakai, Y Kawakatsu, ...
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 60 (3 …, 2017
22017
Time-Optimal Attitude Control Law with a Strategy of Applying to Orbital Control for Spinning Solar Sail Driven by Reflectivity Control
K Oguri, R Funase
Advances in the Astronautical Sciences 158, 933-951, 2016
22016
Reliable and robust implementation of attitude determination and control subsystem and initial flight operation results of 50-kg-class interplanetary spacecraft PROCYON
T Ito, S Ikari, T Nakatani, M Fujimoto, K Ariu, K Oguri, T Inamori, R Funase, ...
International Symposium on Space Flight Dynamics (ISSFD) 2015, 2015
22015
EQUULEUS Trajectory Design
K Oguri, K Oshima, S Campagnola, K Kakihara, N Ozaki, N Baresi, ...
The Journal of the Astronautical Sciences, 1-27, 2020
12020
SRP-Based Orbit Control with Application to Orbit Stationkeeping at Small Bodies
K Oguri, JW McMahon
Advances in the Astronautical Sciences 168 (2), 2077-2093, 2019
12019
EQUULEUS: Mission to Earth-Moon Lagrange Point by a 6U Deep Space CubeSat
S Ikari, N Ozaki, S Nakajima, K Oguri, K Miyoshi, S Campagnola, ...
12017
Solar Radiation Pressure–Based Orbit Control with Application to Small-Body Landing
K Oguri, JW McMahon
Journal of Guidance, Control, and Dynamics 43 (2), 195-211, 2020
2020
Autonomous Guidance for Robust Achievement of Science Observations around Small Bodies
K Oguri, JW McMahon
AAS Guidance, Navigation, and Control conference, 2020
2020
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Articles 1–20