Attitude estimation and control using linearlike complementary filters: theory and experiment
L Benziane, A El Hadri, A Seba… - … on Control Systems …, 2016 - ieeexplore.ieee.org
This brief proposes new algorithms for attitude estimation and control, based on fused
inertial vector measurements using a linear complementary filters principle. First, n-order …
inertial vector measurements using a linear complementary filters principle. First, n-order …
Attitude estimation & control of autonomous aerial vehicles
L Benziane - 2015 - theses.hal.science
Nowadays, we see a growing popularity of the use of Unmanned Aerial Vehicles (UAV)
ofespecially Vertical Take-Off and Landing (VTOL) type. One of the most known VTOL is …
ofespecially Vertical Take-Off and Landing (VTOL) type. One of the most known VTOL is …
[PDF][PDF] Nonlinear automatic control of the satellites by using the quaternion and the angular velocities' vectors
R Lungu, M Lungu, M Ioan - INCAS Bulletin, 2015 - academia.edu
In this paper, the authors propose a new architecture for the control of the satellites' attitude
by using a control law mainly based on a proportional-integrator component with respect to …
by using a control law mainly based on a proportional-integrator component with respect to …