https://nova.newcastle.edu.au/vital/access/ /manager/Index en-au 5 https://nova.newcastle.edu.au/vital/access/ /manager/Repository/uon:48340 input-to-state stability property. Then, we establish an attitude deviation system with an output feedback normal form that has a strict vector relative degree of unity. This enables us to achieve robust output regulation based on an internal model. In particular, we can construct a high-gain stabilizer for the relevant augmented system. As a major consequence, our study achieves not only precision attitude tracking with exponential convergence but also the input-to-state stability disturbance attenuation for the closed-loop system. Finally, we show extensive simulation and experimental results to illustrate the approach. Corrigendum to: Robust precision attitude tracking of an uncertain rigid spacecraft based on regulation theory (International Journal of Robust and Nonlinear Control, (2019), 29, 11, (3666-3683), 10.1002/rnc.4578)]]> Tue 14 Mar 2023 17:29:45 AEDT ]]> https://nova.newcastle.edu.au/vital/access/ /manager/Repository/uon:48804 Thu 06 Apr 2023 16:10:40 AEST ]]> https://nova.newcastle.edu.au/vital/access/ /manager/Repository/uon:32069 Fri 27 Apr 2018 11:24:50 AEST ]]> https://nova.newcastle.edu.au/vital/access/ /manager/Repository/uon:32984 Fri 17 Aug 2018 15:43:56 AEST ]]>