The Application of Computer Simulation to Flexible Spacecraft Dynamics

Zhao Jun ,  Xiao You Zhang ,  Yong De Jin

ICEIC : International Conference on Electronics, Informations and Communications

1995 .01

The Application of computer Simulation to Flexible Spacecraft Dynamics

Zhao Jun ,  Zhang Xiaoyou ,  Jin Yongde

ICEIC : International Conference on Electronics, Informations and Communications

1995 .08

Optimal State Feedback Control for Large Angle Maneuver of Flexible Spacecraft

Daesik Kim ,  Chunhwey Kim ,  Hyochoong Bang

대한전자공학회 학술대회

1997 .11

A Robust Control Approach for Maneuvering a Flexible Spacecraft

Yoon Gyeoung Sung ,  Jea Won Lee ,  Hun Mo Kim

KSME International Journal

2001 .02

유연성을 고려한 인공위성 자세제어

정보환 ,  박순기

대한전자공학회 학술대회

1997 .11

유연성을 고려한 인공위성 자세제어 ( Attitude Control of Spacecraft with Flexible Modes )

정보환 ,  박순기

대한전자공학회 학술대회

1997 .11

Dynamic Output Feedback Regulation of Robots with Flexible Joints

Young I. Son ,  Hyungbo Shim ,  Nam H. Jo 외 1명

제어로봇시스템학회 국제학술대회 논문집

2002 .10

Spacecraft Environment Interaction Studies in Japan

Mengu Cho ,  Yasuhi ,  o Akahoshi 외 4명

한국항공우주학회 학술발표회 초록집

2010 .04

Research Progress of the Structure Vibration-Attitude Coordinated Control of Spacecraft

Jingyu Yang ,  Shiying Qu ,  Jiahui Lin 외 10명

International Journal of Aeronautical and Space Sciences

2015 .12

Three-axis Attitude Control for Flexible Spacecraft by Lyapunov Approach under Gravity Potential

Hyochoong Bang ,  Kwang-Hyun Lee ,  Hyung-Chul Lim

International Journal of Aeronautical and Space Sciences

2003 .05

On Lagrangian Approach to Mixed H₂/H_∞ Control Problem : The State Feedback Case

Kwang-Hyun Cho ,  Jong-Tae Lim

Journal of Electrical Engineering and information Science

1996 .03

Attitude estimation: with or without spacecraft dynamics?

Yang ,  Yaguang ,  Zhou 외 1명

Advances in aircraft and spacecraft science

2017 .01

Dynamics and Control of a Large Spacecraft with Flexible Appendages in Gravitational Field

Masahi ,  o Nohmi ,  Masa 외 1명

제어로봇시스템학회 국내학술대회 논문집

1995 .10

Robust and Optimal Attitude Control Law Design for Spacecraft with Inertia Uncertainties

Yonmook Pa ,  k ,  Min-Jea Tahk

International Journal of Aeronautical and Space Sciences

2002 .11

The design of power electronics in the spacecraft

Eui-Chan Kim ,  Sang-Kon Lee

정보 및 제어 논문집

2012 .10

ADAPTIVE OPTIMAL OUTPUT FEEDBACK CONTROL

신형철 ,  변증남

대한전기학회 학술대회 논문집

1981 .07

Output Feedback Control of Flexible Rotor Bearing System Subject to Periodic Disturbances

김종선 ,  이종원

대한기계학회 춘추학술대회

1988 .01

LMI Based H_∞ Active Vibration Control of a Structure with Output Feedback

Y. B. Kim ,  J. H. Byun ,  H. J. Jeong 외 2명

한국동력기계공학회 학술대회 논문집

1999 .06

Problem Issues of Development Thermal Protection Systems for Spacecraft

P. V. Nikitin

International Symposium on Transport Phenomena in Thermal Engineering

1993 .05

Numerical analysis of the attitude stability of a charged spacecraft in the Pitch-Roll-Yaw directions

Yehia A. Abdel-Aziz ,  Muhammad Shoaib

International Journal of Aeronautical and Space Sciences

2014 .03