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Missile two-loop acceleration autopilot design based on 1 Missile tw-loop acc leration autopilot design based 1 L adaptive output feedback control
| Content Provider | Semantic Scholar |
|---|---|
| Author | Shao-Ming, He |
| Copyright Year | 2014 |
| Abstract | This article documents the design of a novel two-loop acceleration autopilot based on 1 L adaptive output feedback control for tail-controlled missiles. The inner loop is an adaptive angle-of-attack tracking loop and the outer loop is the traditional PI controller for error compensation. A systematic low-pass filter design procedure is provided for minimum phase system and is applied to the inner loop design while the parameters of the outer loop are obtained from the multi-objective optimization problem. The effectiveness of the proposed autopilot is verified through numerical simulations under various conditions. |
| File Format | PDF HTM / HTML |
| Alternate Webpage(s) | http://ocean.kisti.re.kr/downfile/volume/ksass/HGJHC0/2014/v15n1/HGJHC0_2014_v15n1_74.pdf |
| Language | English |
| Access Restriction | Open |
| Content Type | Text |
| Resource Type | Article |
