Performance analysis of proportional navigation, neoclassical and pseudoclassical guidance methods on a 6DOF missile modelHodžić, Mirza (Avtor) Prljača, Naser (Avtor) PNpseudoclassical navigationneoclassical navigation6DOFmissile guidanceProportional navigation (PN) is a missile guidance law usually used for low maneuvering targets. PN generates a commanding lateral acceleration normal to the Line of Sight (LOS) which commands the missile to steer toward a target. PN is determined by measauring the LOS angular velocity. For a maneuvering target, PN yields a non-zero final miss distance. The advanced guidance laws such as integrated guidance and control (IGC) or optimal missile guidance yield better results, but are much more difficult to implement. The paper presents variants of the traditional PN, which offer a similar result but require only the measurement of the LOS rate. The guidance laws are simualted on a 6DOF dynamic model and the results are compared with those obtained with the traditional PN guidance law.20252026-06-22 13:32:38Neznano183936UDK: 004.85:629.056.8ISSN pri članku: 0013-5852COBISS_ID: 280332035sl