Problem 2:An athlete, starting from rest, pulls handle A to the left with a constant force of P = 150 [N].Knowing that after the handle A has been pulled 0.5 [m], its velocity is 5 [m/s] to the left,determine:a) A position constraint equation using the given coordinate system.b) An acceleration constraint equation.c) The acceleration of A using kinematics equations.d) The acceleration of B using your constraint equation.e) How much weight (magnitude) the athlete is lifting in pounds using Newton's 2nd Law.You must draw a FBD and KD of the circled assembly, assuming the pulleys aremassless. Note: 1 [lbf] = 4.448 [N].ХАУв

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Answered: Problem 2: An athlete, starting from…

Principles of Heat Transfer (Activate Learning with these NEW titles from Engineering!)

8th Edition

ISBN:9781305387102

Author:Kreith, Frank; Manglik, Raj M.

Publisher:Kreith, Frank; Manglik, Raj M.

Chapter1: Basic Modes Of Heat Transfer

Section: Chapter Questions

Problem 1.3DP

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For the Following question Graph all 4 : [I just need all 4 graphs and please explain and make clean solution] Position vs time Velocity vs time Acceleration vs time Force vs time [For your convenience, I have solved the numerical solutions for the problem] (Please Look at the picture since it is much cleaner) Question : A 550 kilogram mass initially at rest acted upon by a force of F(t) = 50et Newtons. What are the acceleration, speed, and displacement of the mass at t = 4 second ? a =(50 e^t)/(550 ) [N/kg] v = ∫_0^t▒(50 e^t )dt/(550 )= v_0 +(50 e^t-50)/550=((e^t- 1))/11 x = ∫_0^t▒(e^t- 1)dt/(11 )= x_0 +(e^t- t - 1)/(11 ) a(4s)=(50*54.6)/550= 4.96[m/s^2 ] v(4s)=((e^4-1))/11= 4.87[m/s] x(4s)=((e^4- 4 - 1))/11= 4.51 [m]
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Need only a handwritten solution only (not a typed one).
2.1.28. [Level 2] In the year 2137 a hovering spacecraft releases a probe in the atmosphere far above the surface of New Earth, a planet orbiting Alpha Proximi. The gravita- tional acceleration g1 is constant and equal to 7.5 m/s?. How far will the probe have traveled when it has reached 98% of its terminal speed? The probe's speed is governed by ÿ = -g1 + cy where y is the probe's position above the planet's surface (expressed in m). c = 1.2 × 10-4 m-1.
Please assist with this question. I reviewed the lecture notes that was given and do not understand. Please answer with a detailed explanation. Thank you. I believe there is an easier way to solve this using matlab apparently but I dont know. I will have an image of the reference slide.
You walk along the beach towards a dock while your friend rows a boat towards the same dock on a flat lake. Your friend's boat approaches the dock on a straight course, but also rotates about its center-of-mass since your friend is not pulling evenly on the oars. If you knew your own velocity (vwalker), the magnitude of boat's angular velocity (thetaboat), and radius vector from yourself to your friend in the boat (rfriend) at any given time, you could use the following equation to calculate the your friend's velocity: vfriend = vwalker + (thetaboat)k x rfriend where k is a unit vector in the vertical direction. True False
21. The programmer uses three-point method for UT[2] setup for a sharp-tip pointer. If the programmer recorded each of three-points by precisely contacting the sharp-tip to the tip of the stationary reference pointer on the table, then (a) UT[2] setup is accurate (b) UT[2] setup is not accurate (c) the accuracy of UT[2] setup is still uncertain 22. User frame UF[3] is accurately set up on the part reference surface which is unparallel to the surface where the robot is mounted. To jog the robot TCP to move perpendicularly to the part reference surface, the programmer (a) needs to select World jogging coordinate system (b) needs to activate UF[3] and select User Frame jogging coordinate system
(b): Let us first consider controlling the orbit of deputy spacecraft to rendezvous with chief spacecraft. Define x = [r] and x = x = R to represent the deputy orbital state and its target (= chief orbit) in Cartesian coordinates, respectively. The control input is thruster acceleration, u € R³, in the ECI frame. Denote the relative state by dx = x-x. Table 2 summarize the initial orbital elements. Table 2: Keplerian orbital elements at epoch (t = 0) for deputy and chief about Earth (ECI frame) Orbital element Deputy Unit Chief semi-major axis ad = 11500 ac 10000 km eccentricity inclination ed = 0.15 id=35 ee = 0.3 i = 50 degree right ascension of ascending node d = 50 Ως = 50 degree argument of periapsis true anomaly at epoch Wd Vd= 0 = 40 We = 40 degree Ve=0 degree (b.1): Derive the error dynamics of our system in ECI frame under the influence of u. (b.2): Consider a candidate Lyapunov function V = ½dr¹ K₁dr+dv₁dv, where K₁ = K, and K, > 0. Discuss the positive definiteness of V, and…
Question: For The Given 4-DOF Robot: A. Assign Appropriate Frames For The Denavit-... For the given 4-DOF robot: a. Assign appropriate frames for the Denavit-Hartenberg representation. b. Fill out the parameters table. c. Write an equation in terms of A matrices that shows how UTH can be calculated. U # d. a a A1 0-1 A2 1-2 Аз 2 -3 A4 3- H
The subject is Dynamics and Kinematics.
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