Design of a robust controller for the VEGA TVC using the L1-Adaptive Control

Q2 Engineering
Naji Anees Muqdad Naji, Adrian Stoica
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引用次数: 0

Abstract

The purpose of this study is to Design of a robust controller for the VEGA TVC using the L1-Adaptive Control. The performance of the system with an L1 adaptive controller has been compared with that of a classical controller. The L1 adaptive controller optimization is an efficient as well as an effective approach for the design of a robust controller. The L1 adaptive controller ensures the robustness of the system against uncertainties, noise, and disturbances[10]. In a launch vehicle parameters like mass, thrust, and aerodynamic properties are time-varying. Due to the time-varying nature of these parameters gain scheduling is necessary with the classical control design methods otherwise the closed-loop system might become unstable for some values of these parameters. This procedure is costly and has no robustness. In addition to this, there are external disturbances also which can make the control system unstable. This is the reason why robust control is necessary. There is a trade-off between achievable performance and robustness. So, we need to compromise between required performance and robustness as per the requirement.
利用 L1 自适应控制为 VEGA TVC 设计鲁棒控制器
本研究的目的是利用l1 -自适应控制为VEGA TVC设计一个鲁棒控制器。并将L1自适应控制器与经典控制器的性能进行了比较。L1自适应控制器优化是一种有效的鲁棒控制器设计方法。L1自适应控制器确保了系统对不确定性、噪声和干扰的鲁棒性[10]。在运载火箭中,质量、推力和空气动力学特性等参数是随时间变化的。由于这些参数的时变特性,在经典控制设计方法中,增益调度是必要的,否则在这些参数的某些值下闭环系统会变得不稳定。这个过程成本高,而且没有鲁棒性。除此之外,外部干扰也会使控制系统不稳定。这就是为什么需要鲁棒控制的原因。在可实现的性能和健壮性之间存在权衡。因此,我们需要根据需求在所需的性能和健壮性之间做出妥协。
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来源期刊
INCAS Bulletin
INCAS Bulletin Engineering-Aerospace Engineering
自引率
0.00%
发文量
50
审稿时长
8 weeks
期刊介绍: INCAS BULLETIN is a scientific quartely journal published by INCAS – National Institute for Aerospace Research “Elie Carafoli” (under the aegis of The Romanian Academy) Its current focus is the aerospace field, covering fluid mechanics, aerodynamics, flight theory, aeroelasticity, structures, applied control, mechatronics, experimental aerodynamics, computational methods. All submitted papers are peer-reviewed. The journal will publish reports and short research original papers of substance. Unique features distinguishing this journal: R & D reports in aerospace sciences in Romania The INCAS BULLETIN of the National Institute for Aerospace Research "Elie Carafoli" includes the following sections: 1) FULL PAPERS. -Strength of materials, elasticity, plasticity, aeroelasticity, static and dynamic analysis of structures, vibrations and impact. -Systems, mechatronics and control in aerospace. -Materials and tribology. -Kinematics and dynamics of mechanisms, friction, lubrication. -Measurement technique. -Aeroacoustics, ventilation, wind motors. -Management in Aerospace Activities. 2) TECHNICAL-SCIENTIFIC NOTES and REPORTS. Includes: case studies, technical-scientific notes and reports on published areas. 3) INCAS NEWS. Promote and emphasise INCAS technical base and achievements. 4) BOOK REVIEWS.
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