This course trains you in the skills needed to program specific orientation and achieve precise aiming goals for spacecraft moving through three dimensional space. First, we cover stability definitions of nonlinear dynamical systems, covering the difference between local and global stability. We then analyze and apply Lyapunov's Direct Method to prove these stability properties, and develop a nonlinear 3-axis attitude pointing control law using Lyapunov theory. Finally, we look at alternate feedback control laws and closed loop dynamics.
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Spacecraft Dynamics and Control 专项课程科罗拉多大学波德分校课程信息
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第 3 门课程（共 4 门）
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完成时间大约为31 小时
英语（English）
字幕：法语（French）, （欧洲人讲的）葡萄牙语, 俄语（Russian）, 英语（English）, 西班牙语（Spanish）
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可分享的证书
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100% 在线
立即开始，按照自己的计划学习。
第 3 门课程（共 4 门）
高级
完成时间大约为31 小时
英语（English）
字幕：法语（French）, （欧洲人讲的）葡萄牙语, 俄语（Russian）, 英语（English）, 西班牙语（Spanish）
对员工进行热门技能培训能否为您的公司带来益处？
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科罗拉多大学波德分校
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完成时间为 4 小时
Nonlinear Stability Definitions
Discusses stability definitions of nonlinear dynamical systems, and compares to the classical linear stability definitions. The difference between local and global stability is covered.
完成时间为 4 小时
12 个视频 （总计 67 分钟）
完成时间为 5 小时
Overview of Lyapunov Stability Theory
Lyapunov's direct method is employed to prove these stability properties for a nonlinear system and prove stability and convergence. The possible function definiteness is introduced which forms the building block of Lyapunov's direct method. Convenient prototype Lyapunov candidate functions are presented for rate- and state-error measures.
完成时间为 5 小时
14 个视频 （总计 129 分钟）
完成时间为 11 小时
Attitude Control of States and Rates
A nonlinear 3-axis attitude pointing control law is developed and its stability is analyized using Lyapunov theory. Convergence is discussed considering both modeled and unmodeled torques. The control gain selection is presented using the convenient linearized closed loop dynamics.
完成时间为 11 小时
8 个视频 （总计 82 分钟）
完成时间为 10 小时
Alternate Attitude Control Formulations
Alternate feedback control laws are formulated where actuator saturation is considered. Further, a control law is presented that perfectly linearizes the closed loop dynamics in terms of quaternions and MRPs. Finally, the 3-axis Lyapunov attitude control is developed for a spacecraft with a cluster of N reaction wheel control devices.
完成时间为 10 小时
6 个视频 （总计 97 分钟）
审阅
- 5 stars81.96%
- 4 stars9.83%
- 3 stars4.91%
- 2 stars3.27%
来自CONTROL OF NONLINEAR SPACECRAFT ATTITUDE MOTION的热门评论
由 DA 提供Sep 18, 2020
Excellent course but it could have been smoother if the instructor kept himself in loop with people doing the course
由 SD 提供Feb 3, 2018
Excellent teaching from Professor Schaub ! Course has been very well organised and touches on the important aspects of nonlinear control. Looking forward to more courses from you.
Thank you !
由 SH 提供Sep 11, 2020
Thanks Prof Schaub, that was a wonder of a course! Learned so much and still want to proceed :)
由 PP 提供Nov 26, 2020
The whole course is really good. The instructor is awesome at teaching concepts. I got to learn a lot of new things.
关于 Spacecraft Dynamics and Control 专项课程
Spacecraft Dynamics and Control covers three core topic areas: the description of the motion and rates of motion of rigid bodies (Kinematics), developing the equations of motion that prediction the movement of rigid bodies taking into account mass, torque, and inertia (Kinetics), and finally non-linear controls to program specific orientations and achieve precise aiming goals in three-dimensional space (Control). The specialization invites learners to develop competency in these three areas through targeted content delivery, continuous concept reinforcement, and project applications.
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