PROBLEM 5 Exercises of Machine Dynamics & System Dynamics Problem 5 1. Determine the velocity and the acceleration of a particle in Cartesian coordinates described by the following coordinate vector: r(t) q(t) = ϕ(t) , z(t) x(t) k(t) = y(t) z(t) Note: • Begin with the relationship between the Cartesian coordinates k(t) and the cylindrical coordinates q(t). Solution Given x(t) r cos ϕ cos ϕ − sin ϕ 0 r k(t) = y(t) = r sin ϕ = sin ϕ cos ϕ 0 0 z(t) z 0 0 1 z considering for simplicity r = r(t), ϕ = ϕ(t) then the velocity is given as ṙ cos ϕ − rϕ̇ sin ϕ v(t) = ṙ sin ϕ + rϕ̇ cos ϕ ż cos ϕ − sin ϕ 0 vr = sin ϕ cos ϕ 0 vϕ 0 0 1 vz with vr = ṙ vϕ = rϕ̇ vz = ż Note: The velocity vector amplitude does not chang by changing the coordinate system used to descript the velocity vector therefore kCartesian v (t)k2 = kCylindrical v (t)k2 The acceleration is given as r̈ cos ϕ − ṙϕ̇ sin ϕ − ṙϕ̇ sin ϕ − rϕ̇2 cos ϕ − rϕ̈ sin ϕ a(t) = r̈ sin ϕ + ṙ ϕ̇ cos ϕ + ṙ ϕ̇ cos ϕ − r ϕ̇2 sin ϕ + r ϕ̈ cos ϕ z̈ r̈ cos ϕ − 2ṙϕ̇ sin ϕ − rϕ̇2 cos ϕ − rϕ̈ sin ϕ = r̈ sin ϕ + 2ṙϕ̇ cos ϕ − rϕ̇2 sin ϕ + rϕ̈ cos ϕ z̈ cos ϕ − sin ϕ 0 ar = sin ϕ cos ϕ 0 aϕ 0 0 1 az SS2016 - 3.ed Exercises of Machine Dynamics & System Dynamics so with ar = r̈ − rϕ̇2 aϕ = 2ṙϕ̇ + rϕ̈ az = z̈ SS2016 - 3.ed PROBLEM 5 PROBLEM 6 Exercises of Machine Dynamics & System Dynamics Problem 6 Sometimes it is easier to describe the motion on a curved path in cylindrical coordinates than in Cartesian coordinates. The position vector in cylindrical coordinates is: r(t) = r(t)er + z(t)ez Whereas the unit vector er depends on the angle ϕ and this on its part again depends on the time, which can be written as er = er (ϕ(t)) Due to this time dependence of the unit vector, the derivation with respect to time for the velocity and the acceleration are not as simple expressions as in Cartesian coordinates. Determine these expressions? Z Z0 P ez r(t) eφ ey Y er ex φ r X Solution Given r(t) = r(t)er + z(t)ez SS2016 - 3.ed PROBLEM 6 Exercises of Machine Dynamics & System Dynamics with r(t) = r and z(t) = z. Then we could write r(t) = rer + zez Considering the coordinates shown in the next figure eφ ey er φ φ ex we have the following er = cos ϕex + sin ϕey eϕ = − sin ϕex + cos ϕey derivating these two equations for time we get ėr = −ϕ̇ sin ϕex + ϕ̇ cos ϕey ėϕ = ϕ̇ sin ϕex + cos ϕey = ϕ̇eϕ = −ϕ̇ cos ϕex − ϕ̇ sin ϕey = −ϕ̇ cos ϕex − sin ϕey = −ϕ̇er This final result is very important ėr = ϕ̇eϕ ėϕ = −ϕ̇er The velocity is calculated such as d (r(t)) dt = ṙer + rėr + żez = ṙer + rϕ̇eϕ + żez = vr er + vϕ eϕ + vz ez v(t) = SS2016 - 3.ed Exercises of Machine Dynamics & System Dynamics where vr = ṙ vϕ = rϕ̇ vz = ż The acceleration is given as d (v(t)) dt = r̈er + ṙėr + ṙϕ̇eϕ + rϕ̈eϕ + rϕ̇ėϕ + z̈ez = r̈er + ṙϕ̇eϕ + ṙϕ̇eϕ + rϕ̈eϕ − rϕ̇2 er + z̈ez a(t) = = r̈ − rϕ̇2 er + (2ṙϕ̇ + rϕ̈) eϕ + z̈ez = ar er + aϕ eϕ + az ez where ar = r̈ − rϕ̇2 aϕ = 2ṙϕ̇ + rϕ̈ az = z̈ SS2016 - 3.ed PROBLEM 6 PROBLEM 7 Exercises of Machine Dynamics & System Dynamics Problem 7 Using the chain rule of differentiation we get: a(t) = r̈(t) = J rq q̈(t) + K rq q̇ Q Determine K rq and q̇ Q . Solution ṙ = v = J rq q̇ = m X ∂r i=1 ∂qi q̇i a = v̇ = r̈ " m X ∂ = i=1 ∂t = m X " i=1 = m X ∂ ∂t q̇i i=1 ∂r q̇i ∂qi !# ! ∂r ∂r ∂ q̇i q̇i + ∂qi ∂qi ∂t m X ∂ 2 r ∂qj ∂qi ∂qj ∂t j=1 ! # ∂r + q̈i ∂qi with m = 3 = 3 X ∂ 2r ∂ 2r ∂ 2r ∂r q̇i q̇ + q̇ q̇ + q̇ q̇ + q̈ 1 i 2 i 3 i ∂q1 ∂qi ∂q2 ∂qi ∂q3 ∂qi i=1 | ∂qi{z } | {z } | {z } j=1 2 = j=2 j=3 2 2 ∂ r 2 ∂ r ∂r ∂ r q̇ + q̇1 q̇2 + q̇1 q̇3 + q̈1 2 1 ∂q1 ∂q1 ∂q2 ∂q1 ∂q3 ∂q1 ∂ 2r ∂r ∂ 2r ∂ 2r +q̇2 q̇1 + 2 q̇22 + q̇2 q̇3 + q̈2 ∂q2 ∂q1 ∂q2 ∂q2 ∂q3 ∂q2 ∂ 2r ∂ 2r ∂ 2r ∂r + q˙3 q̇1 + q̇3 q̇2 + 2 q̇32 + q̈3 ∂q3 ∂q1 ∂q3 ∂q2 ∂q3 ∂q3 | K {z } q̇ rq Q | {z } J rq q̈ q̇12 2q̇1 q̇2 i 2q̇1 q̇3 ∂2r q̇ 2 ∂q32 2 } 2q̇2 q̇3 q̇32 = h ∂2r ∂q12 ∂2r ∂q1 ∂q2 ∂2r ∂q1 ∂q3 | ∂2r ∂q22 {z K rq ∂2r ∂q2 ∂q3 | + h | ∂r ∂q1 ∂r ∂q2 {z J rq ∂r ∂q3 i } q̈1 q̈2 q̈3 | {z } q̈ SS2016 - 3.ed {z q̇ Q } PROBLEM 8 Exercises of Machine Dynamics & System Dynamics Problem 8 An airplane climbs at a constant speed v and at a constant climb angle β. The airplane is being tracked by a radar station at point A on the ground. Given • H, β, v • Determine the radial velocity Ṙ and the angular velocity θ̇ as functions of the tracking angle θ. Hint For the following figure the law of sines yields R sin SS2016 - 3.ed π +β 2 = vt sin π −θ 2 = H sin (θ − β) Exercises of Machine Dynamics & System Dynamics SS2016 - 3.ed PROBLEM 8 Exercises of Machine Dynamics & System Dynamics Problem 9 Solve the same problem (Problem 8) using the cylindrical coordinates. Given • H, β, v SS2016 - 3.ed PROBLEM 9 Exercises of Machine Dynamics & System Dynamics PROBLEM 10 Problem 10 A robot arm consists of two parts, which are simply supported in point A. The lower part (length L1 ) rotates anti-clockwise with the angular speed ω1 . The upper part (Length L2 ) is powered clockwise by a flanged e ngine a t t he i ntermediate h inge ( angular s peed ω2 ). Given • ω1 • |ω2 | = 2ω1 • θ1 (0), θ2 (0) • L1 , L2 1. Find the position vector I rOP written in the inertia system. 2. Compute the absolute velocity of the tip P in the inertial system using the jacobian, and assuming the angles θ1 (0) and angle θ2 (0) at the time t = 0. 3. Compute the absolute acceleration of the tip P in the inertial system using the K rq and q Q . SS2016 - 3.ed