Inertia-Free Spacecraft Attitude Tracking with Disturbance Rejection and Almost Global Stabilization
By Amit K. Sanyal, Adam M. Fosbury, Nalin A. Chaturvedi, Dennis S. Bernstein. 2009
203 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Control and Systems Engineering
View Paper: https://www.semanticscholar.org/paper/4f109614609ca852f23a62413b913b041a9027cc
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In Aerospace Engineering
In Control and Systems Engineering
Citations in the corpus
- Robust Adaptive Attitude Tracking on ${\rm SO}(3)$ With an Application to a Quadrotor UAV (2013, background): “Compared with [21], the proposed adaptive tracking control system has simpler controller structures, and the proposed robust adaptive tracking control system is applied to a general class of unstructured or nonharmonic uncertainties.”
- Quaternion-Based Hybrid Control for Robust Global Attitude Tracking (2011, unknown): “To express the difference between the reference trajectory , (Rd, ωd), and the actual rigid body trajectory, (R,ω), we mploy a common coordinate transformation that resolves th angular velocity error in the body frame (see [5], [7], [20], [23], [40], [41]).”
- Attitude stabilization of rigid spacecraft with finite‐time convergence (2011, methodology): “In [14], a continuous nonlinear control law for spacecraft attitude tracking is derived based on rotation matrices.”