@inproceedings{86af8f335e9647709936b80c86ae1fe7,
title = "Control limitations on static unstable airframe using two-loop acceleration autopilot",
abstract = "An analysis for controlling a static-unstable tactical missile using two-loop acceleration autopilot was detailed. The rate feedback loop was firstly presented. The equivalent actuator dynamics was introduced and examined. Thus an overall stabilization condition combined with both low and high frequency cases was proposed. The lever effect led by inertial measurement unit was of benefit to a great controllable range. The results show that the autopilot control capacity is dominated by actuator bandwidth, and a compromise should be determined between the flight performance and the actuator requirement for a static unstable tactical missile.",
keywords = "Actuator, Autopilot, Control limitation, Lever effect",
author = "Wang Jiang and Lin, \{De Fu\} and Fan, \{Jun Fang\}",
year = "2012",
doi = "10.4028/www.scientific.net/AMR.383-390.4385",
language = "English",
isbn = "9783037852958",
series = "Advanced Materials Research",
pages = "4385--4390",
booktitle = "Manufacturing Science and Technology",
note = "2011 International Conference on Manufacturing Science and Technology, ICMST 2011 ; Conference date: 16-09-2011 Through 18-09-2011",
}