In this chapter a mathematical model for multi‐party engagement kinematics is derived suitable for developing, implementing, and testing modern missile guidance systems. The model developed is suitable for both conventional and more advanced optimal intelligent guidance, particularly those based on the game theory guidance techniques. The model accommodates changes in vehicle body attitude and other nonlinear effects such as limits on lateral acceleration and may be extended to include aerodynamic effects. The model is found suitable for computer simulation analysis of multi‐party engagements. The chapter considers the derivation of engagement dynamics, whereas derivations of some of the well‐known conventional guidance laws, such as the proportional navigation (PN) and the augmented PN, are given. The model derived in the chapter is referred to as the four degrees‐of‐freedom model as it includes three degrees (x, y, z) of translational motion and one degree of rotational motion.
Four Degrees‐of‐Freedom (DOF) Simulation Model for Missile Guidance and Control Systems
2017-04-25
25 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Tema Archiv | 1984
|Missile Guidance and Control Systems
TIBKAT | 2004
|Missile guidance and control systems
TIBKAT | 2004
|