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To address this issue, a flight control algorithm that employed state space model predictive control (MPC) to suppress the effect of airwake was presented for aircraft landing on the carrier in this article. The MPC controller was built on the basis of the small-disturbance motion equation of a carrier-based aircraft under the landing status. Meanwhile, in particular, the airwake model was introduced in MPC controller so that its influence could be mitigated promptly. The computer simulation experiments demonstrated that the proposed method could effectively reduce the trajectory deviation caused by airwake and improve the success rate of carrier landing.<\/jats:p>","DOI":"10.1177\/0142331218780962","type":"journal-article","created":{"date-parts":[[2018,7,19]],"date-time":"2018-07-19T12:26:26Z","timestamp":1532003186000},"page":"2205-2213","update-policy":"https:\/\/doi.org\/10.1177\/sage-journals-update-policy","source":"Crossref","is-referenced-by-count":18,"title":["Flight control and airwake suppression algorithm for carrier landing based on model predictive control"],"prefix":"10.1177","volume":"41","author":[{"given":"Ke","family":"Tang","sequence":"first","affiliation":[{"name":"School of Instrument Science and Opto-electronics Engineering, Beihang University, China"}],"role":[{"role":"author","vocabulary":"crossref"}]},{"given":"Wei","family":"Wang","sequence":"additional","affiliation":[{"name":"School of Instrument Science and Opto-electronics Engineering, Beihang University, China"}],"role":[{"role":"author","vocabulary":"crossref"}]},{"given":"Yue","family":"Meng","sequence":"additional","affiliation":[{"name":"School of Instrument Science and Opto-electronics Engineering, Beihang University, China"}],"role":[{"role":"author","vocabulary":"crossref"}]},{"given":"Mingyan","family":"Zhang","sequence":"additional","affiliation":[{"name":"School of Instrument Science and Opto-electronics Engineering, Beihang University, China"}],"role":[{"role":"author","vocabulary":"crossref"}]}],"member":"179","published-online":{"date-parts":[[2018,7,19]]},"reference":[{"issue":"3","key":"bibr1-0142331218780962","first-page":"645","volume":"24","author":"Deng J","year":"2012","journal-title":"Journal of System Simulation"},{"issue":"3","key":"bibr2-0142331218780962","first-page":"235","volume":"33","author":"Froisy JB","year":"1994","journal-title":"Computers & Chemical Engineering"},{"issue":"18","key":"bibr3-0142331218780962","first-page":"5940","volume":"21","author":"Geng J","year":"2009","journal-title":"Journal of System Simulation"},{"key":"bibr4-0142331218780962","unstructured":"Hariharapura RS (2015) Automatic carrier landing system for V\/STOL aircraft using L1 adaptive and optimal control."},{"key":"bibr5-0142331218780962","unstructured":"Heffley RK (1990) Outer-loop control factors for carrier aircraft. 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