Title :
Horizontal waypoint guidance design using optimal control
Author_Institution :
Agency for Defense Dev., Taenon
fDate :
7/1/2002 12:00:00 AM
Abstract :
A horizontal waypoint guidance algorithm is proposed by applying line-following guidance to waypoint line segments in sequence. The line-following guidance is designed using an LQR (linear quadratic regulator). Then, the optimal waypoint changing points are derived by minimizing the accelerations required for changing the waypoint line segments. Also derived is a sufficient condition for the stability bound of ground speed changes based on the Lyapunov stability theorem. Simulation results show that the proposed algorithm can effectively guide a vehicle along the sequence of waypoint line segments.
Keywords :
Lyapunov methods; aircraft control; linear quadratic control; military aircraft; missile guidance; stability; LQR; Lyapunov stability theorem; attack directions; ground speed changes; horizontal waypoint guidance algorithm; line-following guidance; linear quadratic regulator; optimal waypoint changing points; stability bound; target location arrival time; terrain masking; threat avoidance; unmanned flying vehicle; waypoint line segments; Acceleration; Algorithm design and analysis; Kinematics; Lyapunov method; Navigation; Optimal control; Regulators; Stability analysis; Sufficient conditions; Vehicles;
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
DOI :
10.1109/TAES.2002.1039430