{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2025,6,18]],"date-time":"2025-06-18T04:15:09Z","timestamp":1750220109000,"version":"3.41.0"},"publisher-location":"New York, NY, USA","reference-count":12,"publisher":"ACM","license":[{"start":{"date-parts":[[2022,6,24]],"date-time":"2022-06-24T00:00:00Z","timestamp":1656028800000},"content-version":"vor","delay-in-days":0,"URL":"https:\/\/www.acm.org\/publications\/policies\/copyright_policy#Background"}],"content-domain":{"domain":["dl.acm.org"],"crossmark-restriction":true},"short-container-title":[],"published-print":{"date-parts":[[2022,6,24]]},"DOI":"10.1145\/3548608.3559293","type":"proceedings-article","created":{"date-parts":[[2022,10,14]],"date-time":"2022-10-14T17:47:01Z","timestamp":1665769621000},"page":"713-716","update-policy":"https:\/\/doi.org\/10.1145\/crossmark-policy","source":"Crossref","is-referenced-by-count":0,"title":["Gust Load Alleviation by L1 Adaptive Control"],"prefix":"10.1145","author":[{"given":"Ao","family":"He","sequence":"first","affiliation":[{"name":"School of Aeronautics, Northwestern Polytechnical University, China"}],"role":[{"role":"author","vocabulary":"crossref"}]},{"given":"Ban","family":"Wang","sequence":"additional","affiliation":[{"name":"School of Aeronautics, Northwestern Polytechnical University, China"}],"role":[{"role":"author","vocabulary":"crossref"}]},{"given":"Shanshan","family":"Zhang","sequence":"additional","affiliation":[{"name":"School of Aeronautics, Northwestern Polytechnical University, China"}],"role":[{"role":"author","vocabulary":"crossref"}]},{"given":"Zhenghong","family":"Gao","sequence":"additional","affiliation":[{"name":"School of Aeronautics, Northwestern Polytechnical University, China"}],"role":[{"role":"author","vocabulary":"crossref"}]}],"member":"320","published-online":{"date-parts":[[2022,10,14]]},"reference":[{"key":"e_1_3_2_1_1_1","volume-title":"Investigation of the Helios Prototype Aircraft Mishap. Volume 1: Mishap Report","author":"Brown T. E.","year":"2004","unstructured":"Noll, T. E. , Brown , J. M. , Perez-Davis , M. E. , Ishmael , S. D. , Tiffany , G. C. and Gaier , M. , \u201c Investigation of the Helios Prototype Aircraft Mishap. Volume 1: Mishap Report \u201d, 2004 . Noll, T. E., Brown, J. M., Perez-Davis, M. E., Ishmael, S. D., Tiffany, G. C. and Gaier, M., \u201cInvestigation of the Helios Prototype Aircraft Mishap. Volume 1: Mishap Report\u201d, 2004."},{"key":"e_1_3_2_1_2_1","first-page":"428","article-title":"The expanding domain of aeroelasticity[J]","volume":"1946","author":"Collar A","unstructured":"Collar A R . The expanding domain of aeroelasticity[J] . Journal of the Royal Aeronautical Society , 1946 ,50: 428 . Collar A R. The expanding domain of aeroelasticity[J]. Journal of the Royal Aeronautical Society,1946,50:428.","journal-title":"Journal of the Royal Aeronautical Society"},{"key":"e_1_3_2_1_3_1","first-page":"580","article-title":"The present status of aircraft stability problems in the aeroelastic domain[J].","volume":"1959","author":"Taylor A","unstructured":"Taylor A S . The present status of aircraft stability problems in the aeroelastic domain[J]. Journal of the Royal Aeronautical Society , 1959 ,63: 580 . Taylor A S. The present status of aircraft stability problems in the aeroelastic domain[J].Journal of the Royal Aeronautical Society,1959,63:580.","journal-title":"Journal of the Royal Aeronautical Society"},{"key":"e_1_3_2_1_4_1","doi-asserted-by":"crossref","unstructured":"Dillsaver M J Cesnik C E Kolmanovsky I V.Gust load alleviation control for very flexible aircraft[C].AIAA Atmospheric Flight Mechanics Conference Portland Oregon 2011.  Dillsaver M J Cesnik C E Kolmanovsky I V.Gust load alleviation control for very flexible aircraft[C].AIAA Atmospheric Flight Mechanics Conference Portland Oregon 2011.","DOI":"10.2514\/6.2011-6368"},{"key":"e_1_3_2_1_5_1","first-page":"2250","article-title":"Active Control and Wind Tunnel Test Verif ication of Multi-control Surfaces Wing for Gust Alleviation [J]","volume":"2009","author":"Chen Lei","unstructured":"Lei Chen , Zhigang WU , Chao Yang , Changhong Tang , Longfei Chu . Active Control and Wind Tunnel Test Verif ication of Multi-control Surfaces Wing for Gust Alleviation [J] . Journal of Aeronautics , 2009 ,30(12): 2250 - 2256 . Lei Chen, Zhigang WU, Chao Yang, Changhong Tang, Longfei Chu. Active Control and Wind Tunnel Test Verif ication of Multi-control Surfaces Wing for Gust Alleviation [J]. Journal of Aeronautics,2009,30(12):2250-2256.","journal-title":"Journal of Aeronautics"},{"issue":"02","key":"e_1_3_2_1_6_1","first-page":"61","article-title":"Application of LQG control theory in gust load alleviation system [J]","volume":"2007","author":"Zhang Junhong","unstructured":"Junhong Zhang , Zhenshui Li , Mengquan Zhan , Yakui Gao . Application of LQG control theory in gust load alleviation system [J] . Flight Dynamics , 2007 ( 02 ): 61 - 64 . Junhong Zhang, Zhenshui Li, Mengquan Zhan, Yakui Gao. Application of LQG control theory in gust load alleviation system [J]. Flight Dynamics,2007(02):61-64.","journal-title":"Flight Dynamics"},{"key":"e_1_3_2_1_7_1","first-page":"177","article-title":"Approach of Gust Load Alleviation Based on System Nonlinearit[J]","volume":"2020","author":"Yang Jianzhong","unstructured":"Jianzhong Yang , Xianxue Qin , Shibin Yang , Dan Xu . Approach of Gust Load Alleviation Based on System Nonlinearit[J] . Computer Measurement and Control , 2020 ,28(07): 177 - 181 +187. Jianzhong Yang, Xianxue Qin, Shibin Yang, Dan Xu. Approach of Gust Load Alleviation Based on System Nonlinearit[J]. Computer Measurement and Control,2020,28(07):177-181+187.","journal-title":"Computer Measurement and Control"},{"key":"e_1_3_2_1_8_1","first-page":"157","article-title":"The Dynamic Properties\u3000and\u3000Control\u3000Method of a Flying Wing with High Aspect-Ratio and Strong Coupling Between Aeroelasticity and Flight Dynamic[J]","volume":"2020","author":"Zhang Shuo","unstructured":"Shuo Zhang , Zhengjie Wang , Hao Chen . The Dynamic Properties\u3000and\u3000Control\u3000Method of a Flying Wing with High Aspect-Ratio and Strong Coupling Between Aeroelasticity and Flight Dynamic[J] . Journal of Beijing Institute of Technology , 2020 ,40(02): 157 - 162 . Shuo Zhang, Zhengjie Wang, Hao Chen. The Dynamic Properties\u3000and\u3000Control\u3000Method of a Flying Wing with High Aspect-Ratio and Strong Coupling Between Aeroelasticity and Flight Dynamic[J]. Journal of Beijing Institute of Technology,2020,40(02):157-162.","journal-title":"Journal of Beijing Institute of Technology"},{"key":"e_1_3_2_1_9_1","volume-title":"Investigation The Problem in Multidisciplinary Design of High Altitude Long Endurance Unmanned Aerial Vehicle [D]","author":"Sun Zhiwei","year":"2016","unstructured":"Zhiwei Sun . Investigation The Problem in Multidisciplinary Design of High Altitude Long Endurance Unmanned Aerial Vehicle [D] . Northwestern Polytechnical University , 2016 . Zhiwei Sun. Investigation The Problem in Multidisciplinary Design of High Altitude Long Endurance Unmanned Aerial Vehicle [D]. Northwestern Polytechnical University, 2016."},{"key":"e_1_3_2_1_10_1","volume-title":"Study on lateral control law for unmanned aerial vehicle based on L1 adaptive algorithm[J]","author":"Wang Junling","year":"2019","unstructured":"Junling Wang , Chengbo Yu , Jie Zhou , Zhida Yang . Study on lateral control law for unmanned aerial vehicle based on L1 adaptive algorithm[J] . Journal of Harbin University of Commerce (Natural Science Edition) , 2019 , 35(02):214-218. Junling Wang, Chengbo Yu, Jie Zhou, Zhida Yang. Study on lateral control law for unmanned aerial vehicle based on L1 adaptive algorithm[J]. Journal of Harbin University of Commerce (Natural Science Edition), 2019, 35(02):214-218."},{"key":"e_1_3_2_1_11_1","volume-title":"L1 Adaptive Control Law for Attitude of Rocket[A]","author":"Su Xiujian","year":"2019","unstructured":"Xiujian Su , Guoqiang Wu , Congyuan He , Wenya Zhou . L1 Adaptive Control Law for Attitude of Rocket[A] . Chinese Society of Aeronautics and Astronautics . 2019 )Fourth(Proceedings of China Aviation Science and Technology Conference [C]. Chinese Society of Aeronautics and Astronautics: Chinese Society of Aeronautics and Astronautics, 2019: 7. Xiujian Su, Guoqiang Wu, Congyuan He, Wenya Zhou. L1 Adaptive Control Law for Attitude of Rocket[A]. Chinese Society of Aeronautics and Astronautics.2019)Fourth(Proceedings of China Aviation Science and Technology Conference [C]. Chinese Society of Aeronautics and Astronautics: Chinese Society of Aeronautics and Astronautics, 2019:7."},{"key":"e_1_3_2_1_12_1","doi-asserted-by":"publisher","DOI":"10.2514\/1.27606"}],"event":{"name":"ICCIR 2022: 2022 2nd International Conference on Control and Intelligent Robot","acronym":"ICCIR 2022","location":"Nanjing China"},"container-title":["Proceedings of the 2022 2nd International Conference on Control and Intelligent Robotics"],"original-title":[],"link":[{"URL":"https:\/\/dl.acm.org\/doi\/10.1145\/3548608.3559293","content-type":"unspecified","content-version":"vor","intended-application":"text-mining"},{"URL":"https:\/\/dl.acm.org\/doi\/pdf\/10.1145\/3548608.3559293","content-type":"unspecified","content-version":"vor","intended-application":"similarity-checking"}],"deposited":{"date-parts":[[2025,6,17]],"date-time":"2025-06-17T18:10:38Z","timestamp":1750183838000},"score":1,"resource":{"primary":{"URL":"https:\/\/dl.acm.org\/doi\/10.1145\/3548608.3559293"}},"subtitle":[],"short-title":[],"issued":{"date-parts":[[2022,6,24]]},"references-count":12,"alternative-id":["10.1145\/3548608.3559293","10.1145\/3548608"],"URL":"https:\/\/doi.org\/10.1145\/3548608.3559293","relation":{},"subject":[],"published":{"date-parts":[[2022,6,24]]},"assertion":[{"value":"2022-10-14","order":2,"name":"published","label":"Published","group":{"name":"publication_history","label":"Publication History"}}]}}