Application of a second-order sliding mode observer, which is based on the nonlinear dynamic sliding manifold, as a nonlinear uncertain system estimator in the homing (terminal guidance) loop with augmented proportional navigation guidance is demonstrated. It is shown that sliding mode observers have an advantage over traditional Kalman filters in the homing loop upon target maneuvering at a short time-to-go.
Effect of sliding mode observers in the homing guidance loop
01.02.2005
9 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Effect of sliding mode observers in the homing guidance loop
Online Contents | 2005
|Sliding Mode Estimation Scheme for Missile Homing Guidance
British Library Conference Proceedings | 1995
|Adaptive Sliding-Mode Guidance of a Homing Missile
AIAA | 1999
|