Title :
Capture region of 3D PPN guidance law for intercepting high speed target
Author_Institution :
Dept. of Aerosp. Eng., Tamkang Univ., Tamsui, Taiwan
Abstract :
The implementation of a classic three dimensional PPN guidance against a high speed-nonmaneuvering target is analyzed. All the analysis is performed in a line of sight fixed coordinate. By utilizing an auxiliary function inspired from the tangential relative velocity at interception, a necessary and sufficient condition for the airfoil shape capture region for intercepting the target is obtained. In addition, a sufficient condition for the capture region with the finite line of sight turn rate constraint is also presented.
Keywords :
missile guidance; target tracking; 3D PPN guidance law; airfoil shape capture region; high speed nonmaneuvering target; high speed target interception; tangential relative velocity; turn rate constraint; Aerodynamics; Automotive components; Computer vision; Equations; Lyapunov method; Missiles; Navigation; Performance analysis; Shape; Sufficient conditions;
Conference_Titel :
Decision and Control, 2009 held jointly with the 2009 28th Chinese Control Conference. CDC/CCC 2009. Proceedings of the 48th IEEE Conference on
Conference_Location :
Shanghai
Print_ISBN :
978-1-4244-3871-6
Electronic_ISBN :
0191-2216
DOI :
10.1109/CDC.2009.5399631
