Title :
L+2, an improved line of sight guidance law for UAVs
Author :
Curry, Renwick ; Lizarraga, Mariano ; Mairs, Bryant ; Elkaim, Gabriel Hugh
Author_Institution :
Dept. of Comput. Eng., Univ. of California Santa Cruz, Santa Cruz, CA, USA
Abstract :
This paper describes a new guidance law that extends the pursuit guidance law previously developed by Park et. al. Several improvements are presented that allow operation in the real world. A stability analysis accounts for the dynamic response of the bank angle commands which leads to the definition of regions of instability. Another extension accounts for situations where the pursuit aim point is not defined by the previous work. A third extension changes the pursuit distance-to-go from a constant to a constant time-to-go so that the linearized transient response is independent of ground speed. Yet another extension defines a “homing” mode in which the UAV flies to a goal point without a defined path, commonly used as a “return-to-base,” either as a safety measure or as an end-of-mission order. Since there is no constraint that the goal point be stationary, we demonstrate that the new law can be used to follow a moving target whose location is known, such as a mobile ground control station. Simulations with a 6 degree-of-freedom aircraft model demonstrate these features.
Keywords :
autonomous aerial vehicles; stability; transient response; 6 degree-of-freedom aircraft model; L+2; UAV; bank angle command dynamic response; constant time-to-go; end-of-mission order; homing mode; line of sight guidance law; linearized transient response; mobile ground control station; pursuit distance-to-go; pursuit guidance law; return-to-base; stability analysis; Acceleration; Aircraft; Atmospheric modeling; Stability analysis; Trajectory; Vectors; Vehicles;
Conference_Titel :
American Control Conference (ACC), 2013
Conference_Location :
Washington, DC
Print_ISBN :
978-1-4799-0177-7
DOI :
10.1109/ACC.2013.6579804