ArticleGust Alleviation by Active–Passive Combined Control of the Flight Platform and Antenna Array for a Flying Wing SensorCraft

Author:

Hao Shuai12,Ma Tielin3,Wang Yi4,Li Huadong1,Zhao Shiwei1,Tan Puxue5

Affiliation:

1. School of Aeronautic Science and Engineering, Beihang University, Beijing 100191, China

2. Hiwing General Aviation Equipment Co., Ltd., Beijing 100074, China

3. Research Institute of Unmanned Systems, Beihang University, Beijing 100083, China

4. AVIC (Chengdu) UAS Co., Ltd., Chengdu 611000, China

5. School of Engineering, University of Liverpool, Liverpool L693BX, UK

Abstract

SensorCraft is an intelligence, surveillance, and reconnaissance (ISR) system that integrates unmanned flight platforms and airborne antenna arrays. Under gust loads, the high–aspect–ratio, light–wing structure of SensorCraft has considerable bending and torsion deformation, affecting the flight performance of unmanned flight platforms and leading to the loss of antenna arrays’ electromagnetic performance. Taking SensorCraft as the background, a wing conformal antenna array was designed, an aircraft model with a passive wingtip device was established, a control law was developed by the LQG/LTR method, and a gust alleviation active–passive combined control method of a “LQG/LTR active controller + passive wingtip device” was proposed. By constructing an unsteady aerodynamic reduced–order model (ROM) based on the Volterra series and a conformal array pattern fast method based on the modal form, the effectiveness of the gust alleviation active–passive combined control method on the aircraft platform and antenna array was analyzed. The results show that structural deformation of the wing conformal antenna leads to changes in the main lobe gain, beam direction, and sidelobe level. The active–passive gust alleviation method has obvious advantages. Compared with the LQG/LTR active gust alleviation method, the peak value of wingtip displacement is reduced by 15.6%, and the peak value of the gain loss is reduced by 0.72 dB, which is conducive to better performance of the airborne conformal antenna array.

Funder

National Natural Science Foundation of China

Publisher

MDPI AG

Subject

Aerospace Engineering

Reference25 articles.

1. Cord, T., and Newbern, S. (2001, January 10–17). Unmanned air vehicles: New challenges in design. Proceedings of the Aerospace Conference, Big Sky, MT, USA.

2. Hall, J.K., and Clark, C.S. (2002). SensorCraft Mission Simulation Study, Air Force Research Laboratory, Wright–Patterson AFB OH Air Vehicles Directorate.

3. Genello, G.J., Baldygo, W.J., and Callahan, M.J. (2001, January 10–17). Modeling and simulation for Sensor Craft multi–mission radar. Proceedings of the Aerospace Conference, Big Sky, MT, USA.

4. Smallwood, B., Canfield, R., and Terzuoli, A. (2003, January 7–13). Structurally integrated antennas on a joined–wing aircraft. Proceedings of the 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Norfolk, VA, USA.

5. Vartio, E., Shaw, E., and Vetter, T. (2008, January 18–21). Gust load alleviation flight control system design for a SensorCraft vehicle. Proceedings of the 26th AIAA Applied Aerodynamics Conference, Honolulu, HI, USA.

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3