授课教师：Ossmann Daniel

国籍：德国

职称：教授

教师简介（中英文）：Ossmann Daniel教授目前在德国慕尼黑应用科学大学担任控制工程全职教授， AIAA 高级会员，MDPI Aerospace 期刊编辑委员会成员，欧洲嵌入式控制协会会员，Automatica, Control Engineering Practice, IEEE TAC, IEEE Control Systems Letters等国际顶级期刊的审稿人。Daniel教授分别在2006年和2008年获得航空工程和机械工程双硕士学位。2008曾任职于德国航空航天中心（DLR）飞行系统研究所，从事飞行测试工程师。在DLR 的系统动力学与控制研究所进行飞行器的故障诊断与容错控制工作的研究。参与了欧盟 EU-FP7 的重大研究项目 ADDSAFE (2009-2012) 和 RECONFIGURE (2013-2016) ，项目中所提出的算法，提高了飞机的可持续性和性能。2015年在明尼苏达大学航空航天工程与力学系做博士后，为大学建设了先进的风力涡轮机减载控制实验平台。2017年回到德国DLR系统动力学与控制研究所，从事现代飞控、FDI以及鲁棒控制技术的研究， 并参与了欧盟地平线 2020 项目FLEXOPT，负责开发主动颤振抑制演示验证器。2021 年 10 月 1 日起成为德国慕尼黑应用科学大学的高级研究型教授。

Ossmann Daniel is the full professor for control systems at the Munich University of Applied Sciences HM. He is reviewer for Automatica, Control Engineering Practice, IEEE TAC, IEEE Control Systems Letters, member of editor board for MDPI Aerospace, affiliate member of the European Embedded Control Institute, senior member of the AIAA. Prof. Daniel receive two Masters in Aviation (2006) and in Mechanical Engineering with focus on Control and Automation (2008) . He joined the Institute of Flight System of the German Aerospace Center early 2008. Located at the airfield in Manching he worked as flight test engineer specialized on Handling Quality evaluations for military aircraft. His research focus on model based Fault Detection as well as Fault Tolerant Control. In the two EU-FP 7 research projects ADDSAFE (2009-2012) and RECONFIGURE (2013-2016) , he developed together with AIRBUS and other academic partners advanced algorithms to improve aircraft sustainability and performance. In 2015, he joined the Aerospace Engineering and Mechanics Department at the University of Minnesota as Postdoctoral Associate. Besides supervising students and teaching undergraduate and graduate courses his research focused on robust control techniques with application to wind turbines. He was deigned and tested advanced load reduction control algorithms for the university owned 2.5MW Clipper wind turbine. In May 2017 he returned DLR's Institute of System Dynamics and Control working on modern flight control algorithms, FDI, and modern robust control techniques. He was involved in the Clean Sky Project NACOR to develop load alleviation algorithms for aircraft as well as the Horizon 2020 project FLEXOPT to develop a demonstrator for active flutter suppression.

In September 2019, he started my position as full professor for control engineering at the Munich University of Applied Sciences HM (Hochschule München). Since October 1st, 2021 he officially hold a Research Professorship at HM.

课程简介（中英文）：这门课是工程控制论的入门课程， 侧重原理，其内容密切结合工程实际，是一门专业基础课，而且也是科学方法论之一。课程主要介绍经典控制理论方面的基础知识以及“控制论”(Cybernetics)在航空航天工程中的应用。 从控制的概念入手讲述如何将已知的物理关系转化为系统输入/输出行为的微分方程。 然后，利用拉普拉斯变换推导传递函数并理解图代数的思想， 引导学生将理解传递函数的极点与相应的动态行为之间的关系。课程的第二部分侧重于如何为线性单输入单输出系统设计简单的线性控制器， 讨论控制器设计面临的相互矛盾的目标（精度、速度、阻尼、干扰抑制、导引行为等）时，如何从工程角度出发设计控制器。 本课程将辅以 Matlab/Simulink 中的示例，因此通过对这门课程的学习，要求学生学会运用控制理论的基本原理和思想方法，初步学会分析和研究机、电、液系统中信号的传递、反馈与控制，以及机、电、液系统的动态特性，并结合后续专业课的学习，为将来在解决一些实际控制工程问题打下一定的基础。

An introduction to the idea of control is given at the beginning of the lecture. Then, the goal is to translate known physical relationships into differential equations for the I/O behavior of a system and learn about the basic system types. Then we make use of the Laplace transform to derive transfer functions and understand the idea of the block diagram algebra. Students will gather an understanding of the relationship between the poles of a transfer function and the corresponding dynamic behavior, especially with respect to stability. The second part of the lecture focuses on the design of simple, linear controllers for linear single-input, single-output systems. The conflicting goals of controller design (accuracy, speed, degree of damping, disturbance suppression, guidance behavior) are discussed. The lecture is supported with examples in Matlab/Simulink so students can directly use their gathered knowledge and implement in simple software code.