PPT-Gyroscopic attitude control systems

Stepan Tkachev Introduction Attitude control systems Passive Active Gravitational Magnetic Magnetic Gyroscopic Thrusters Introduction Attitude control systems Need fields Independent. Gyroscope. Group Presenters:. 1. . Wahaj. Ahmad. 2. Hassan Baber. 3. . Mujtaba. . Abbas. 4. . Hassaan. Tariq. Overview. Introduction.. Precessional angular motion.. Gyroscopic couple.. 1. Attitude Instrument Flying . Attitude Instrument flying involves aircraft control by reference to its instruments rather than outside visual references. 2. Three Fundamental Skills. Skills. Instrument cross-check. N.C.Townsend. . Faculty of Engineering and the Environment . nick@soton.ac.uk. Fluid Structure Interactions Research Group. Acknowledgement: . This project is supported by . The Lloyd’s Register Educational Trust.. MECHANICAL DEPARTMENT. 5. th. . SEMESTER. . PREPARED . BY:. . . . . GUIDED . BY. : . JEET . PAREKH (130030119569. ). . . . . Describe the . four types of airspeed.. Describe the . meaning of the white arc on the ASI.. Describe the . upper limit of the white arc (VFE). . Describe VNE. What is . the . indication on the ASI . Dr. Imtiaz Hussain. email: . imtiaz.hussain@faculty.muet.edu.pk. URL :. http://imtiazhussainkalwar.weebly.com/. Lecture-1. Introduction to Subject . &. Review of Basic Concepts of Classical control. University of Waterloo. Outline. Faculty members. Overview. Examples. Courses available. Faculty Members. Faculty members in the ECE Control Systems Group include:. D. Davison. A. . . Heunis. D. . Module Leader: Dr Muhammad . Arif. Email: . muhammadarif. 13. @hotmail.com. Batch: . 10. BM . Year: . 3. rd. Term: . 2. nd. . Credit Hours (Theory): . 4. Lecture Timings: Monday (. 12:00-2:00. ) and Wednesday (. What does a decrease in pressure cause the altimeter to indicate? . Which pressure(s) is felt at the Airspeed Indicator?. Describe the two types of information the VSI provides. . What happens to the VSI when the pilot pulls back on the yoke/stick?. Module Leader: Dr Muhammad . Arif. Email: . muhammadarif. 13. @hotmail.com. Batch: . 10. BM . Year: . 3. rd. Term: . 2. nd. . Credit Hours (Theory): . 4. Lecture Timings: Monday (. 12:00-2:00. ) and Wednesday (. Balloonsat. Team Members. Project Manager. Benjamin Anderson. Assistant Project Manager. Patrick . Deskin. Electrical Subsystem Lead. Brigette. Cochran. Team Member. Chad . Reinart. Previous Team Members. ME 343 Control Systems Fall 2009Solution of State Space Equation426We consider the linear time-invariant systemAnd we solve to obtainSolution by the Laplace TransformWe Laplace transform the state equ Roger D. Werking Head, Attitude Determination and Control Section National Aeronautics and Space Administration/ Goddard Space Flight Center Extensiye work has been done for many years in the areas of attitude determination, attitude prediction, and attitude control. During this time, it has been difficult to obtain reference material that provided a comprehensive overview of attitude support activities. This lack of reference material has made it difficult for those not intimately involved in attitude functions to become acquainted with the ideas and activities which are essential to understanding the various aspects of spacecraft attitude support. As a result, I felt the need for a document which could be used by a variety of persons to obtain an understanding of the work which has been done in support of spacecraft attitude objectives. It is believed that this book, prepared by the Computer Sciences Corporation under the able direction of Dr. James Wertz, provides this type of reference. This book can serve as a reference for individuals involved in mission planning, attitude determination, and attitude dynamics an introductory textbook for stu dents and professionals starting in this field an information source for experimen ters or others involved in spacecraft-related work who need information on spacecraft orientation and how it is determined, but who have neither the time nor the resources to pursue the varied literature on this subject and a tool for encouraging those who could expand this discipline to do so, because much remains to be done to satisfy future needs. one. . Dr. Adil . ABed. Nayeeif . 2019-2020. Gyroscopic Couple and . Precessional. . Motion. Precessional. Angular Motion. We have already discussed that the angular acceleration is the rate of change of .