A Study on Coordinated Attitude Flying for Sequential Spacecraft Tracking
نویسندگان
چکیده
منابع مشابه
Attitude Tracking Control for Spacecraft Formation Flying
We develop a non-linear tracking control law to be applied to formation flying spacecraft. Each spacecraft in the formation is modeled as a rigid body with N axisymmetric wheels controlled by axial torques, and the kinematics are represented by Modified Rodriques Parameters (MRPs). The paper first derives the open-loop reference attitude, rate, and acceleration commands for tracking a moving ob...
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ژورنال
عنوان ژورنال: Journal of the Korean Society for Aeronautical & Space Sciences
سال: 2009
ISSN: 1225-1348
DOI: 10.5139/jksas.2009.37.1.028