Sliding mode based integrated pitch-yaw acceleration autopilot design for varying-velocity missile

A. Awad, H. Wang. Sliding mode based integrated pitch-yaw acceleration autopilot design for varying-velocity missile. In 12th IEEE International Conference on Control and Automation, ICCA 2016, Kathmandu, Nepal, June 1-3, 2016. pages 104-109, IEEE, 2016. [doi]

Authors

A. Awad

This author has not been identified. Look up 'A. Awad' in Google

H. Wang

This author has not been identified. It may be one of the following persons: Look up 'H. Wang' in Google