Guidance Laws For Impact Angle Constraints And Exo-Atmospheric Engagements

Guidance Laws For Impact Angle Constraints And Exo-Atmospheric Engagements

This thesis deals with development of guidance laws for advanced applications. Two class of guidance problems, namely, impact angle constrained guidance and pulsed guidance for exo-atmospheric engagements, are considered here. Three impact angle constrained guidance schemes are developed using (i) P...

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Bibliographic Details
Main Author: Ratnoo, Ashwini
Other Authors: Ghose, Debasish
Language:en_US
Published: 2010
Subjects:
Guided Aircraft System
Guided Missile
Impact Angle Constraint
Exoatmospheric Constraint
Propotional Navigation Guidance (PNG) Law
State Dependent Riccati Equation Technique
Geometric Guidance Law
Exo-atmospheric Engagements
Pulsed Guidance Law
Lateral Impact
Impact Angle Constrained Trajectories
Military Engineering
Online Access:http://hdl.handle.net/2005/929

Internet

http://hdl.handle.net/2005/929

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