Satellite Attitude Control by Quaternion-Based Backstepping

By Raymond Kristiansen, Per Johan Nicklasson, Jan Tommy Gravdahl. IEEE Transactions on Control Systems Technology, 2005

315 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Control and Systems Engineering

View Paper: https://www.semanticscholar.org/paper/4a763cb77a5331845b1af64cfed98d6ce974dec0

How researchers see this paper

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In Aerospace Engineering

1. Youmin Zhang
2. Qinglei Hu
3. Bing Xiao

In Control and Systems Engineering

1. Bing Xiao
2. Youmin Zhang
3. Qinglei Hu

Citations in the corpus

• Adaptive Sliding Mode Fault Tolerant Attitude Tracking Control for Flexible Spacecraft Under Actuator Saturation (2012, background): “…the design of attitude controlis treating with uncertainties and external disturbances that spacecraft will encounter in operation, and this problem has been extensively studied in the literature based on several inspired control approaches, such as H-infinity control [1], [2], feedback…”
• Quaternion-Based Hybrid Control for Robust Global Attitude Tracking (2011, unknown): “[22]–[25]) is used in Limited circulation.”
• Mathematical modeling and control of a hexacopter (2013, methodology): “A novel PD control, based on quaternions, is here presented, differing from classical approaches based on internal linearization, Lyapunov method or least square estimations, [12], [8], [23].”