A GES attitude observer with single vector observations
From MaRDI portal
Publication:1941266
DOI10.1016/j.automatica.2011.07.005zbMath1260.93026OpenAlexW2142003981WikidataQ59325517 ScholiaQ59325517MaRDI QIDQ1941266
Pedro Batista, Carlos Silvestre, Paulo J. Oliveira
Publication date: 12 March 2013
Published in: Automatica (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.automatica.2011.07.005
Related Items
Attitude estimation by multiplicative exogenous Kalman filter ⋮ Global attitude estimation using single delayed vector measurement and biased gyro ⋮ Attitude, body-fixed Earth rotation rate, and sensor bias estimation using single observations of direction of gravitational field ⋮ Observers for invariant systems on Lie groups with biased input measurements and homogeneous outputs ⋮ On the attitude estimation of nonholonomic wheeled mobile robots ⋮ A geometric framework for rigid body attitude estimation ⋮ Tightly coupled long baseline/ultra-short baseline integrated navigation system ⋮ Globally exponentially stable attitude observer with Earth velocity estimation ⋮ Attitude observer on the special orthogonal group with Earth velocity estimation ⋮ Linear observed systems on groups ⋮ Globally exponentially stable attitude and gyro bias estimation with application to GNSS/INS integration
Cites Work
- A nonlinear position and attitude observer on SE(3) using landmark measurements
- Global optimal attitude estimation using uncertainty ellipsoids
- Intrinsic Observer-Based Stabilization for Simple Mechanical Systems on Lie Groups
- The attitude control problem
- Robust adaptive LQ control schemes
- Nonlinear Complementary Filters on the Special Orthogonal Group
- A coupled nonlinear spacecraft attitude controller and observer with an unknown constant gyro bias and gyro noise
- Pose estimation using line-based dynamic vision and inertial sensors
- Almost-Global Tracking of Simple Mechanical Systems on a General Class of Lie Groups
- Rigid-Body Attitude Control
- A topological obstruction to continuous global stabilization of rotational motion and the unwinding phenomenon
