Flight Path Angle Steering with Lambert Guidance Reference

R Zardashti؛ M Bagherian

دوره 2، شماره 2 ، تیر 1388، ، صفحه 75-79

چکیده
  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 position and velocity obtained by Lambert technique need to be followed in actual flight. In this paper the Flight Path angle Steering (FPS) procedure is used to accomplish the tracking of nominal parameters. The numerical simulations indicate that the integrated procedure is a cost-effective ...  بیشتر