Robust trajectory tracking for a scale model autonomous helicopter
By Robert E. Mahony, Tarek Hamel. 2004
234 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Control and Systems Engineering
View Paper: https://www.semanticscholar.org/paper/655f5d0139ab7da35dfc2fb0719720dce3c169d2
How researchers see this paper
The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.
In Aerospace Engineering
- Farid Kendoul
- Manuel Gil Ortega
- Francisco Rodriguez Rubio
- Guilherme Vianna Raffo
- Tarek Hamel
- Robert E. Mahony
- Frank L. Lewis
- Abhijit Das
In Control and Systems Engineering
- Farid Kendoul
- Frank L. Lewis
- Tarek Hamel
- Robert E. Mahony
- Abhijit Das
- Kamesh Subbarao
- Nicolas Guenard
- Manuel Gil Ortega
Citations in the corpus
- Backstepping Approach for Controlling a Quadrotor Using Lagrange Form Dynamics (2009, methodology): “Reference [13] discussed the robust trajectory tracking of a Lagrangian quadrotor model using backstepping control and proved the stability for any given but bounded trajectory.”
- Real-Time Nonlinear Embedded Control for an Autonomous Quadrotor Helicopter (2007, background): “Therefore, designers often focus on a specific problem, thereby resulting in various techniques such as the differential-flatness approach [10–12], backstepping methodology [5,13], adaptive control [14], robust control [15], small-gain methods [1], etc.”
- Robust Nonlinear Control for Path Tracking of a Quad‐Rotor Helicopter (2015, methodology): “Backstepping approaches applied to the quadrotor helicopter are found in [17,16,15,11,23].”
- Aerial Manipulation: A Literature Review (2018, background): “into account a hierarchical architecture [13], [14] highlighting a time-scale separation between the linear (slow time-scale) and angular (fast time-scale) dynamics.”
- Landing a VTOL Unmanned Aerial Vehicle on a Moving Platform Using Optical Flow (2012, methodology): “For a miniature VTOL UAV in quasi-stationary flight, one can reasonably assume that the aerodynamic forces are always in direction e3 , since the thrust force predominates over other components [20].”
- A Practical Visual Servo Control for an Unmanned Aerial Vehicle (2008, methodology): “The vehicle considered is equipped with an Inertial Measurement Unit (IMU) and an explicit complementary (cid:2)lter is used to provide (cid:2)ltered estimates of attitude [16] and angular velocity for the vehicle.”