DocumentCode
2616821
Title
Trajectory planning for a quadrotor helicopter
Author
Bouktir, Y. ; Haddad, M. ; Chettibi, T.
Author_Institution
Lab. of Struct. Mech., Algiers
fYear
2008
fDate
25-27 June 2008
Firstpage
1258
Lastpage
1263
Abstract
A simple direct method able to generate time-optimal trajectories for a micro quadrotor helicopter is presented. It is based on modeling the quadrotor trajectory as a composition of a parametric function P(lambda) defining the quadrotor path, and a monotonically increasing function lambda(t), specifying the motion on this path. The optimal evolutions of P(lambda) and lambda(t), which are approximated using B-spline functions, are found using a nonlinear optimization technique. The proposed method accounts for the most important constraints inherent to the system behavior, such as underactuation, obstacles avoidance and limits on actuator torques and speeds.
Keywords
aerospace control; collision avoidance; helicopters; nonlinear programming; splines (mathematics); B-spline function; actuator speed; actuator torque; microquadrotor helicopter; nonlinear optimization; obstacles avoidance; optimal evolution; parametric function; quadrotor trajectory; time-optimal trajectories; trajectory planning; unmanned air vehicles; Helicopters; Linear feedback control systems; Motion control; Nonlinear dynamical systems; Predictive models; Robots; Sliding mode control; Trajectory; Unmanned aerial vehicles; Vehicle dynamics; dynamics; nonlinear optimization; quadrotor; trajectory;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Automation, 2008 16th Mediterranean Conference on
Conference_Location
Ajaccio
Print_ISBN
978-1-4244-2504-4
Electronic_ISBN
978-1-4244-2505-1
Type
conf
DOI
10.1109/MED.2008.4602025
Filename
4602025
Link To Document