Modeling & Simulations, Assignments of Mathematical Methods

Newtonian mechanics is kind of powerful tool that can be used to describe any terrestrial or heavenly body's movements. One powerful demonstration of Newtonian mechanics is explaining planetary movements. There exist nine planets around the Sun. Therefore, the constitution of the planetarium can be shown to obey Newtonian mechanics. Furthermore, the following mathematical description attached to this assignment can be shown to describe a mathematical model of the Orbital parameters of planets.

Typology: Assignments

2022/2023

Uploaded on 12/30/2023

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Q01)
Consider the motion of a simple pendulum shown in the Figure 01 and answer the following
questions given in below.
(a) Describe a suitable assumption set that you considered investigating the lost less motion
of the simple pendulum.
โ€ข Negligible air resistance: Assume that the pendulum moves in a vacuum or an
environment with minimal air resistance.
โ€ข Perfectly elastic support: Assume the support (pivot point) of the pendulum is
frictionless and perfectly elastic, with no energy losses.
โ€ข Small angle approximation: Assume the angle of displacement is small, allowing the
use of the small-angle approximation sin(ฮธ) โ‰ˆ ฮธ.
(b) Derive a differential equation to describe the lost-less motion of the simple pendulum.
๐ผ๐‘‘2๐œƒ
๐‘‘2๐œƒ = โˆ’๐‘š๐‘”๐ฟsin๐œƒ
where:
I is the moment of inertia of the pendulum bob,
ฮธ is the angular displacement,
t is time,
m is the mass of the bob,
g is the acceleration due to gravity,
L is the length of the pendulum.
(c) Obtained the solution of the differential equation.
The above differential equation is a nonlinear second-order differential equation.
For small-angle approximation (sinฮธโ‰ˆฮธ), it can be linearized and solved. The solution is
typically in the form:
๐œƒ(๐‘ก) = ๐œƒ0cos(โˆš๐‘”
๐ฟ๐‘ก + ๐œ™)
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Q01)

Consider the motion of a simple pendulum shown in the Figure 01 and answer the following questions given in below. (a) Describe a suitable assumption set that you considered investigating the lost less motion of the simple pendulum.

  • Negligible air resistance: Assume that the pendulum moves in a vacuum or an environment with minimal air resistance.
  • Perfectly elastic support: Assume the support (pivot point) of the pendulum is frictionless and perfectly elastic, with no energy losses.
  • Small angle approximation: Assume the angle of displacement is small, allowing the use of the small-angle approximation sin(ฮธ) โ‰ˆ ฮธ. (b) Derive a differential equation to describe the lost-less motion of the simple pendulum. ๐ผ

= โˆ’๐‘š๐‘”๐ฟsin๐œƒ where: I is the moment of inertia of the pendulum bob, ฮธ is the angular displacement, t is time, m is the mass of the bob, g is the acceleration due to gravity, L is the length of the pendulum. (c) Obtained the solution of the differential equation. The above differential equation is a nonlinear second-order differential equation. For small-angle approximation (sinฮธโ‰ˆฮธ), it can be linearized and solved. The solution is typically in the form:

๐œƒ(๐‘ก) = ๐œƒ 0 cos(โˆš

๐‘” ๐ฟ

where

๐œƒ 0 is the initial displacement,

๐‘” ๐ฟ is the angular frequency, t is time, and ฯ• is the phase angle. (d) Modify the above differential equation for pendulum moves through the air. Damping term in the equation for air resistance, resulting in a modified differential equation:

๐‘‘ 2 ๐œƒ ๐‘‘ 2 ๐œƒ

= โˆ’๐‘š๐‘”๐ฟsin๐œƒ โˆ’ ๐ถ

๐‘‘๐œƒ ๐‘‘๐œƒ where c is the damping coefficient. (e)Explain the energy loss of the pendulum using the solution of the differential equation.

The additional term, โˆ’๐ถ

๐‘‘๐œƒ ๐‘‘๐œƒ in the modified equation represents the damping force due to air resistance. As the pendulum oscillates, energy is decipated as heat through air resistance, causing a gradual decrease in amplitude over the time. (f) Use MATLAB to plot your results and differentiate the motions in different cases of solutions obtained for motions of the pendulum. % Constants m = 1; % mass k = 1; % spring constant A = 1; % amplitude C_values = [0, 0.5]; % damping coefficients (C=0 for lossless, C=0.5 for friction loss)

Figure 01 Q2) Newtonian mechanics is kind of powerful tool that can be used to describe any terrestrial or heavenly body's movements. One powerful demonstration of Newtonian mechanics is explaining planetary movements. There exist nine planets around the Sun. Therefore, the constitution of the planetarium can be shown to obey Newtonian mechanics. Furthermore, the following mathematical description attached to this assignment can be shown to describe a mathematical model of the Orbital parameters of planets. In more, I have attached a kind of mathematical model of the simulation of MATLAB codes and its typical simulation for the Orbital parameters of the Earth. All other orbital parameters of the planets including Earth can be shown in the following table.

Table 01 Table 01: a is the distance of the major axis from the center and e is the eccentricity of the Elliptical Orbits, while Omega is the angular speed for orbits around the sun. (a) Explain the provided mathematical model for each step of the derivation in your own words (b) Extend the MATLAB simulation for 9 planets and attach your simulated model with the answer script. (Hint: assume the initial position for planets with zero angles) Q03) (1) Answer the following questions based on your knowledge of linear systems (a) Briefly explain the Linear system theory (LST) by using its properties of obeying. (b) Provide the input-output relationship of the linear system in the time domain (c) Briefly explain the bilateral Laplace transformed in general (d) Derived the statement for linear gain of a linear system (2) Consider the step-by-step derivation of the input-output relationship for the following RCL circuit in the Figure 02.

Figure 03 (3) Use the Bode plot command in MATLAB to simulate the transfer function of the filter and identify its filter type. (4) Explain the effect for the filter, when a portion of output current injects to the path of the input current using a bypass capacitor C2 across the R2.