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This undergraduate course builds upon the dynamics content of Unified Engineering, a sophomore course taught in the Department of Aeronautics and Astronautics at MIT.
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English
English [CC]
FREE
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Description
ector kinematics are applied to translation and rotation of rigid bodies. Newtonian and Lagrangian methods are used to formulate and solve equations of motion. Additional numerical methods are presented for solving rigid body dynamics problems. Examples and problems describe applications to aircraft flight dynamics and spacecraft attitude dynamics.
Course content
- Aerospace Dynamics Unlimited
- Coriolis “Demystified” Unlimited
- Introduction to Multiple Intermediate Frames Unlimited
- Momentum, Angular Momentum, and Dynamics of a System of Particles Unlimited
- Numerical Solution of Nonlinear Differential Equations Unlimited
- Lagrange’s Equations Unlimited
- Examples Using Lagrange’s Equations Unlimited
- Virtual Work and the Derivation of Lagrange’s Equations Unlimited
- Friction in Lagrange’s Equations Unlimited
- Kinematics of Rigid Bodies Unlimited
- Rigid Body Dynamics Unlimited
- Axisymmetric Rotations Unlimited
- Gyroscopes Unlimited
- Spacecraft Attitude Dynamics Unlimited
- Aircraft Dynamics Unlimited
- Aircraft Longitudinal Dynamics Unlimited
- Aircraft Lateral Dynamics Unlimited
Instructor
Massachusetts Institute of Technology
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