Optimal Guidance Law Design for Air-to-Air Missiles Intercepting Slow and Highly Maneuverable Targets
Abstract
Optimal Guidance Law Design for Air-to-Air Missiles Intercepting Slow and Highly Maneuverable Targets Nguyen Ngoc Thien1 Abstract This paper presents the design of an optimal guidance law for air-to-air missiles (AAMs) engaging slow and highly maneuverable aerial targets, such as helicopters or unmanned aerial vehicles. Unlike conventional proportional navigation (PN), which is optimized for high-speed […]
Fields of Study & Subjects
Guidance and Control Systems
Spacecraft Dynamics and Control
Military Defense Systems Analysis
Publication details
- Journal / source
- International Journal of Science Architecture Technology and Environment
- Publication date
- 4 January 2026