Robust full-envelope missile autopilot design
Jyh‐Ching Juang, Ching-Fang Lin, J.R. Cloutier, Johnny Evers
Abstract
Jyh‐Ching Juang, Ching-Fang Lin, J.R. Cloutier, Johnny Evers
Abstract
The design of a robust full-envelope autopilot for the HAVE DASH II missile system is delineated. Existing control design methods are examined and integrated to meet the stringent performance requirements of the missile autopilot design.>
OpenAlex reports 1 citations for this work. Citation counts describe recorded attention and do not establish research quality.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
The design of a robust full-envelope autopilot for the HAVE DASH II missile system is delineated. Existing control design methods are examined and integrated to meet the stringent performance requirements of the missile autopilot design.>
Key concepts: Autopilot, Missile, Envelope (radar), Flight envelope, Computer science, Engineering, Control engineering, Aerospace engineering