Search
CSV
RISSpacecraft Coupled Tracking Maneuver Using Sliding Mode Control with Input Saturation
Publisher: American Society of Civil Engineers
Abstract: This paper presents a sliding mode control scheme on for autonomous spacecraft formation flying via a virtual leader state trajectory. The configuration space for a spacecraft is the Lie group SE(3), which is the set of ...
Robust Adaptive Unscented Kalman Filter for Spacecraft Attitude Estimation Using Quaternion Measurements
Publisher: American Society of Civil Engineers
Robust Position and Attitude Control for Spacecraft Formation Flying
Publisher: American Society of Civil Engineers
Abstract: An integrated approach combining a state-dependent Ricatti equation (SDRE) and an extended Kalman filter (EKF) is applied to spacecraft formation flying for robust orbital and attitude maneuvers. The formation flying ...
Kinematically Coupled Relative Spacecraft Motion Control Using the State-Dependent Riccati Equation Method
Publisher: American Society of Civil Engineers
Abstract: This paper presents kinematically coupled relative spacecraft motion control in the close proximity of a tumbling target using the state-dependent Riccati equation method for proximity operation mission. In general, a ...