Ground-based testbeds are critical to develop and test different elements of spacecraft
guidance, navigation, and control subsystems. This paper provides an in-detail description …

This paper presents a new six-degree-of-freedom robotic spacecraft simulator, the Multi-
Spacecraft Testbed for Autonomy Research (M-STAR), for testing formation guidance …

During a spacecraft mission design process, engineers often balance the following three
criteria: science return, optimality in performance, and safety. Given a science criterion …

In this work, we focus on the attitude control problem of an imaging satellite required to
acquire and accurately track a target area on the Earth's surface. The proposed hybrid …

针对航天器质量特性在线辨识问题, 建立了适用于航天器转动惯量辨识的数学模型,
分析了其可辨识性和数据采样时间的影响机理. 基于渐消记忆递推最小二乘辨识理论 …

Satellite design has been harshly constrained by surviving entry into space though the
majority of the satellite's lifetime exists in much calmer conditions. Significant study has …

Advances in space technology and interest toward remote sensing mission have grown in
the recent years, requiring the attitude control subsystems of observation satellites to …