Title :
An optimization design method for control law of lateral navigation
Author_Institution :
China National Aeronautical Radio Electronics, Research Institute, China
Abstract :
Optimize the control law by flight leg to achieve a set of gains will promise a better performance, and which will be the future work.
Conference_Titel :
Digital Avionics Systems Conference (DASC), 2013 IEEE/AIAA 32nd
Conference_Location :
East Syracuse, NY, USA
Print_ISBN :
978-1-4799-1536-1
DOI :
10.1109/DASC.2013.6719644