Impact Angle Guidance Using MinMax Approach
Aerospace sciences (Annual conference)
2019-01-01
22 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Terminal impact angle constrained guidance laws using state-dependent Riccati equation approach
SAGE Publications | 2015
|Terminal impact angle constrained guidance laws using state-dependent Riccati equation approach
Online Contents | 2015
|Practical guidance law controlling impact angle
Online Contents | 2007
|