Estimation of the attitude of a CubeSat under environmental torques

Bărbulescu, Lucian-Florentin; Butu, Alin-Florentin; Marian, Marius; Stinga, Florin

doi:10.1109/icstcc.2017.8107049

Search citation statements

Order By: Relevance

Paper Sections

Select...

Satellite Attitude Control System1

Citation Types

Supporting

Mentioning

Contrasting

Year Published

2022

Publication Types

Select...

Article1

Relationship

Self Cite0

Independent1

Authors

Journals

Cited by 1 publication

(1 citation statement)

References 2 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

“…Remark 4 Considering the natural characteristics of space environmental torques (mainly generated by the Earth gravity gradient, geomagnetic field, aerodynamic drag and solar radiation pressure), one can assume that all these torques are L p norm bounded [28], [29]. Thus condition (3) is reasonable.…”

Section: Satellite Attitude Control Systemmentioning

confidence: 99%

Attitude Regulation With Bounded Control in the Presence of Large Disturbances With Bounded Moving Average

Astolfi

Liu

2022

IEEE/CAA J. Autom. Sinica

View full text Add to dashboard Cite

The attitude regulation problem with bounded control for a class of satellites in the presence of large disturbances, with bounded moving average, is solved using a Lyapunov-like design. The analysis and design approaches are introduced in the case in which the underlying system is an integrator and are then applied to the satellite attitude regulation problem. The performance of the resulting closed-loop systems are studied in detail and it is shown that trajectories are ultimately bounded despite the effect of the persistent disturbance. Simulation results on a model of a small satellite subject to large, but bounded in moving average, disturbances are presented.

show abstract

Section: Satellite Attitude Control Systemmentioning

confidence: 99%