Helicopter Optimal Control after Power Failure Using Comprehensive Dynamic Model
Journal of Guidance, Control, and Dynamics ; 35 , 4 ; 1354-1362
01.07.2012
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
ENGINEERING NOTES - Helicopter Optimal Control After Power Failure Using Comprehensive Dynamic Model
Online Contents | 2012
|Optimal Helicopter Operation Considering Power Failure Possibilities
British Library Conference Proceedings | 1994
|Helicopter Optimal Descent and Landing after Power Loss
NTIS | 1977
|Helicopter optimal descent and landing after power loss
NTRS | 1977
|