Analytical Mechanics for Spacecraft Dynamics
This course is part of Advanced Spacecraft Dynamics and Control Specialization
Instructor: Hanspeter Schaub
What you'll learn
Skills you'll gain
There are 3 modules in this course
Next Lagrange’s equations are developed which still assume a finite set of generalized coordinates, but can be applied to multiple rigid bodies as well. Lagrange multipliers are employed to apply Pfaffian constraints. Finally, Hamilton’s extended principle is developed to allow us to consider a dynamical system with flexible components. Here there are an infinite number of degrees of freedom. The course focuses on how to develop spacecraft related partial differential equations, but does not study numerically solving them. The course ends comparing the presented assumed mode methods to classical final element solutions. The material covered is taking from the book "Analytical Mechanics of Space Systems" available at https://arc.aiaa.org/doi/book/10.2514/4.105210.
Energy Based Equations of Motion
Variational Methods in Analytical Dynamics
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