Quaternion-based finite time control for spacecraft attitude tracking

By Shunan Wu, G. Radice, Yongsheng Gao, Zhao-wei Sun. 2011

136 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Control and Systems Engineering

View Paper: https://www.semanticscholar.org/paper/032f1aca43e1f92428369fffdbb055c7bb3ec210

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Michael I. Friswell
2. Qinglei Hu
3. Boyan Jiang

In Control and Systems Engineering

1. Michael I. Friswell
2. Qinglei Hu
3. Boyan Jiang

Citations in the corpus

• Fixed-Time Attitude Control for Rigid Spacecraft With Actuator Saturation and Faults (2016, methodology): “To overcome this limitation, finite-time controllers [11]–[14] based on the Lyapunov approach have been designed for rigid spacecraft, and some of them can deal with actuator faults [12]–[14] or actuator saturation [13], [14].”