Flight Path Angle Steering with Lambert Guidance Reference

R Zardashti; M Bagherian

Volume 2, Issue 2 , July 2009, , Pages 75-79

Abstract
  In this paper a new guidance technique for ballistic missiles and launch vehicles is proposed. Generally the Lambert guidance is used to generate missile nominal (correlated) parameters through powered flight to put it in a ballistic flight path. Because of uncertainties and undesired factors, the nominal ...  Read More