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

The design of power electronics in the spacecraft

Eui-Chan Kim ,  Sang-Kon Lee

정보 및 제어 논문집

2012 .10

Spacecraft Environment Interaction Studies in Japan

Mengu Cho ,  Yasuhi ,  o Akahoshi 외 4명

한국항공우주학회 학술발표회 초록집

2010 .04

Attitude estimation: with or without spacecraft dynamics?

Yang ,  Yaguang ,  Zhou 외 1명

Advances in aircraft and spacecraft science

2017 .01

비선형 기법을 이용한 인공위성의 자세제어에 관한 연구

신성식 ,  송용규 ,  정도희

제어로봇시스템학회 국내학술대회 논문집

1995 .10

Simulation of Spacecraft Attitude Measurement Data by Modeling Physical Characteristics of Dynamics and Sensors

Hungu Lee ,  Jae-Cheol Yoon ,  Yee-Jin Cheon 외 5명

제어로봇시스템학회 국제학술대회 논문집

2004 .08

Design of Solar Array Simulator for Spacecraft

Gyu Bum Joung ,  Jae-Dong Choi

KIEE International Transactions on Electrical Machinery and Energy Conversion Systems

2002 .06

Problem Issues of Development Thermal Protection Systems for Spacecraft

P. V. Nikitin

International Symposium on Transport Phenomena in Thermal Engineering

1993 .05

Design of Optimal Controllers for Spacecraft Formation Flying Based on the Decentralized Approach

Jonghee Bae ,  Youdan Kim

International Journal of Aeronautical and Space Sciences

2009 .05

Design of Optimal Controllers for Spacecraft Formation Flying based on the Decentralized Approach

Jonghee Bae ,  Youdan Kim

제어로봇시스템학회 국제학술대회 논문집

2008 .10

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

Modelling and simulation of a closed-loop electrodynamic shaker and test structure model for spacecraft vibration testing

Waime ,  Steffen ,  Manzato 외 11명

Advances in aircraft and spacecraft science

2018 .01

Output Feedback Control and Its Application to a Flexible Spacecraft

Yoon-Gyeoung Sung ,  Hae-Ho Joo

International Journal of Precision Engineering and Manufacturing

2000 .12

위성 시뮬레이터의 위성 표준 모델 설계와 Anomaly 분석지원

조성기 ,  이상욱 ,  김재훈 외 1명

한국항공우주학회 학술발표회 초록집

2002 .04

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

An Attitude Determination Algorithm for a Spacecraft Using Nonlinear Filter

Yong Joong Yoon ,  Jae Weon Choi ,  Jang Gyu Lee 외 1명

KSME International Journal

1999 .02

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

유연 위성체 모델링을 통한 강체 위성의 자세 제어기 검증

최한준 ,  이상욱

한국항공우주학회 학술발표회 초록집

1997 .11

Design, Implementation and Validation of the KOMPSAT Spacecraft Simulator

Wan Sik Choi ,  Sanguk Lee ,  Jong Won Eun 외 2명

International Journal of Aeronautical and Space Sciences

2000 .11