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  1. 1.6.2 Systems with Rigid Constraints So far we have found $L = T-V$ to be a suitable Lagrangian for systems of point particles subject to forces derived from a potential.

  2. Exercise 2.1: Rotational kinetic energy Show that the rotational kinetic energy can also be written as: $$ T = \frac{1}{2} I\omega^2\\ $$ where $I$ is the moment of inertia about the line through the center of mass with direction $\hat{\omega}$ and $\omeg…

  3. 2.3 Moments of Inertia The rotational kinetic energy consists of the sum of the kinetic energies of all the constituent particles.

  4. 1.8.4 The Restricted Three-Body Problem Consider two bodies of masses $M_0$ and $M_1$ in circular orbits about their barycenter.

  5. 1.6 How to Find Lagrangians It is possible to work back from Newton’s second law and obtain the Lagrangian $L = T - V$.

  6. 1.6.1 Coordinate Transformations Assume we have a mechanical system whose motion is described by a Lagrangian that depends on time, position and velocities.

  7. 2.2 Kinematics of Rotation The motion of a rigid body about a center of rotation (a body-fixed reference point) is characterized at each point in time by an axis of rotation and a rate of rotation According to Euler’s theorem of rotations, we can go from…

  8. Exercise 1.12: Lagrange’s Equations Compute Lagrange’s equations for the Lagrangians in exercise 1.9 using the Lagrange-equations procedure. a.

  9. Exercise 1.14: Coordinate-independence of Lagrange equations Check that the Lagrange equations for central force motion in polar coordinates and in rectangular coordinates are equivalent.

  10. Exercise 1.13: Higher-derivative Lagrangians a.

  11. Exercise 1.11: Kepler’s third law A Lagrangian suitable for studying the relative motion of two particles, of masses $m_1$ and $m_2$, with potential energy $V$, is: $$ L = \frac{1}{2} m \left(\dot{r}^2 + (r\dot{\phi})^2\right) + V(r) $$ The argument $m$ is

  12. Exercise 1.15: Equivalence

    Exercise 1.15: Equivalence Here we use the p->r conversion function to convert the Lagrangian in rectangular coordinates to polar coordinates (and compare to results from notes and exercise 1.14 where it was computed explicitly). ;; The Coordinate convers…

  13. Exercise 1.16: Central force motion Find Lagrangians for central force motion in three dimensions in rectangular coordinates and in spherical coordinates.

  14. Exercise 1.17: Bead on a helical wire A bead of mass $m$ is constrained to move on a frictionless helical wire.

  15. Exercise 1.19: Two-bar linkage The two-bar linkage shown in the figure below is constrained to move in the plane.

  16. Exercise 1.20: Sliding pendulum Consider a pendulum of length $l$ attached to a support that is free to move horizontally, as shown in the figure.

  17. Exercise 1.18: Bead on a triaxial surface A bead of mass $m$ moves without friction on a triaxial ellipsoidal surface.

  18. Exercise 1.40: Bead on a triaxial surface Consider again the motion of a bead constrained to move on a triaxial surface (exercise 1.18).

  19. 2 Rigid Bodies The polhode rolls without slipping on the herpolhode lying in the invariable plane.

  20. Exercise 1.39: Combining Lagrangians a.

  21. Section 1.11: Summary

    Summary This chapter was primarily introducing the Lagrangian method of analyzing mechanical systems.

  22. 1.10.3 Non-holonomic Systems Systems with constraints that are no integrable are called non-holonomic systems.

  23. 1.10.2 Derivative Constraints In this section we look at a specific type of velocity-dependent constraints, which are “total-time derivatives” of a velocity independent function.

  24. 1.10.1 Coordinate Constraints In the previous section, we showed that for motion of a system with the constraint $\varphi(t, q(t), Dq(t)) = 0$, for stationary action, the path variations, $\eta(t)$, must be tangent to the constraint surface.

  25. 1.10 Constrained Motion When using the Lagrangian method, we may choose the coordinate system that is the most convenient - the number of coordinates may match exactly with the number of degrees of freedom of the system, or we may pick a system that has r…

  26. Exercise 1.38: Properties of $\mathscr{E}$, the Euler-Lagrange Operator Refer to Section 1.9 for more details Let $F$ and $G$ be two Lagrangian-like functions of a local tuple, $C$ be a local-tuple transformation function, and $c$ a constant.

  27. Exercise 1.38: Velocity transformation Use the procedure Gamma-bar to construct a procedure that transforms velocities given a coordinate transformation.

  28. 1.9 Abstraction of Path Functions Note: This section may seem rather dry from its title.

  29. Exercise 1.36: Noether integral Consider motion on an ellipsoidal surface.

  30. 1.8.5 Noether’s Theorem If a dynamical system has a symmetry, a coordinate system can be chosen so that the Lagrangian does not depend on a coordinate associated with the symmetry.

  31. Exercise 1.21: A dumbbell

    Exercise 1.21: A dumbbell In this exercise we will recapitulate the derivation of the Lagrangian for constrained systems for a particular simple system.

  32. A coordinate function $\chi$ maps a point in a coordinate patch of a manifold to a coordinate tuple of real numbers: $$ x = \chi(m) $$ where $x$ represents a convenient tuple structure.

  33. Point On A Manifold

    Note: This is just my current understanding while studying Functional Differential Geometry.

  34. Manifolds

    A manifold is a generalization of the idea of a smooth surface embedded in Euclidean space.

  35. This is an easier/less computationally expensive method compared to the one described in Points in a plane using null space.

  36. For two vectors $\vec{a}$ and $\vec{b}$, the cross product $\vec{a} \times \vec{b}$ can be computed using matrix multiplcation1 as: $$ \vec{a} \times \vec{b} = A_\times \vec{b} $$ where $A_\times$ is defined as: $$ A_\times = \begin{bmatrix} 0 & -a_3 & a_…

  37. Bdot attitude controller

    A “bdot” (or $\mathbf{\dot{B}}$) attitude controller is used to detumble a spacecraft using just a magnetometer and torque rods.

  38. The “Hack” computer built during this course has its own instruction set consisting of two instructions: the A-command and the C-command.

  39. All of the chips described in the previous course notes used what is called “combinational logic”, where the output is available instantenously and there is no time-component to their operation.

  40. The Airthmetic and Logic Unit is a core part of a computer based on the Von Neumann architecture.

  41. Two’s complement is a format for representing negative numbers in binary.

  42. Elementary Logic Gates NOT AND OR XOR => output 1 if inputs different MUX: => a, b, sel; if sel == 0: out = a, else: out = b DMUX: => in, sel (outputs a and b): if sel == 0: a = in else b = in 16-bit variants NOT16 : 16 bits in and out AND16 : Two 16-bit…

  43. NAND2Tetris Note 01

    Nand2tetris is a course where we build a full general purpose computer up from basic logic gates - in fact, just NAND gates.

  44. A plane can be defined using its normal vector n.

  45. Allocating torques to RWAs are accomplished by first defining a “distribution matrix” which contains the spin axes of the individual wheels, and then using this matrix to allocate torques.Each column of the distribution matrix consists of the unit vector…

  46. What is TLA+?

    TLA+ is a language for creating “specifications” for computer programs/algorithms and then verify all the possible execution paths and mathematically prove assertions.

  47. Reactions wheels are used for controlling spacecraft attitude to a very high precision.

  48. The TRIAD or Tri-Axial Attitude Determination algorithm is used for attitude determination given two body-frame vectors ($b_1$ and $b_2$) and two corresponding inertial or “reference” frame vectors ($r_1$ and $r_2$).

  49. Used a walkthrough for tips here.

  50. Run the VMs with “Host-Only Networking”.