1 Please answer the best you can. clear; clc; close all;g = 9.81; % [m/s^2] Gravitational accelerationm = 1500; % [kg] Vehicle massb = 35;% [Ns/m] Air drag coefficient1 System modelingDerive an ODE for the velocity of a car on a flat road. Include wind resistance F =-bv. Derive the transfer function from applied force ƒ to velocity v.What is the time constant for the open loop system?f% Create a transfer function P (for "plant") representing the car.% ...% tau = ...P% v_t = ....Do you think the car could reasonably achieve this speed? Why or why not?VWhat is the maximum traction force that the tires can provide without slipping? Look up a reasonable value for the friction coefficientu.% f_max =What is the terminal velocity at maximum traction force?

Transfer Function P(s)=F(s)V(s)=ms+b1Time constant 0.0286Terminal Velocity at maximum traction…

Answered: clear; clc; close all; g = 9.81; %…

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

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secondary spacecraft reference plane primary spacecraft primary orbit plane Once you fix the primary or target spacecraft (the selection of primary spacecraft is only a matter of context), the relative motion of the secondary spacecraft is governed by the following initial value problem: a" 2wy - 3w? a = fz; x (0) = *0, x' (0) = x, y" + 2wa' = fy; y (0) = Yo, Y (0) = % 2' + w? z = fa; z (0) = 20; z' (0) Where w stands for the mean angular velocity of the primary spacecraft within its orbit plane. Also, fy represents the differential acceleration on the secondary spacecraft. fz x (t) Assuming there is no external force acting on the secondary spacecraft, use Laplace Transform to determine its position y (t) in the space. Your z (t) answer will be in terms of w and the set of intial conditions. Hint: The z part of the given IVP is a second order IVP by itself. Therefore it can be solved for z using Laplace Transform. For each of the first two differential equations (from the top), begin…
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Consider a cruise control system shown in Figure 1. Where f is the engine force, v is the velocity, fb is the friction force, and fb = bv. Requirements: Assuming M = 2000 kg, b = 80Nsec/m, and f = 600 N: Find the transfer function of the system.
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汇 Advertised missile performance: Natural Frequency 0.65 a = Angle of attack [rad] q = pitch rate [rad] = 1.25m center of gravity Xcg Zcg = Om center of gravity The equations of motion for the missile are a = q - 0.435sin a + 0.07a -0.00014q q = 111.484(xcg - 1.483)a - (2.2968 - 3.156zcg)q +3.448 + 137895Zcg To acquire the target the missile needs to fly at α = 0.017 [rad] qo= 0 [rad/s] = 0 [rad] So Determine if the missile is stable about the given equilibrium point.
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