American Journal of Aerospace Engineering

Volume 7, Issue 2, December 2020

  • An Optimal Algorithm for Midcourse Guidance Law Under Wind Disturbance

    Sy-Hieu Nguyen, Dinh-Dung Nguyen

    Issue: Volume 7, Issue 2, December 2020
    Pages: 6-15
    Received: 22 March 2020
    Accepted: 8 April 2020
    Published: 31 December 2020
    Abstract: The guidance laws are commonly designed to yield as small a miss distance as possible, harmonious with the missile’s acceleration capability. In recent decades, the concept of optimized guidance law is well understood in applications where information concerning the target range and line-of-sight angle is available. Researchers' efforts have been c... Show More