2019
DOI: 10.3390/sym11101208
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A Closed-Form Expression of the Instantaneous Rotational Lurch Index to Evaluate Its Numerical Approximation

Abstract: The lurch index has recently been introduced in applied kinematics as an integral descriptor of the fluency of the motion of a rigid body in space. It may be defined in different versions, according to the component of motion under investigation. In the present paper, we analyze a rotational lurch index, which describes the fluency of the spin component of motion and whose value depends, through involved relations, on the dynamics of three canonical descriptors of the orientation of a rigid body in space. The … Show more

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Cited by 4 publications
(4 citation statements)
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“…The problem about the order of the numerical schemes, which may be studied either analytically and by means of numerical experiments. The present author has started an analysis of the order of some numerical schemes which rely on ad-hoc Taylor-series-like expansions [46]. It would also be informative to use examples for which the analytic solution is known, and then compare the two numerical solutions to the analytic solution individually.…”
Section: Discussionmentioning
confidence: 99%
“…The problem about the order of the numerical schemes, which may be studied either analytically and by means of numerical experiments. The present author has started an analysis of the order of some numerical schemes which rely on ad-hoc Taylor-series-like expansions [46]. It would also be informative to use examples for which the analytic solution is known, and then compare the two numerical solutions to the analytic solution individually.…”
Section: Discussionmentioning
confidence: 99%
“…The Euler methods are easy to implement on a computing platform, but are the least precise ones. An analysis of the precision of the Euler method on the special orthogonal group was covered in a previous publication of the second author [22]. The precision of the numerical scheme to simulate the dynamics of a flying body be increased by accessing higher-order numerical methods such as those in the Runge-Kutta class.…”
Section: Numerical Methods To Simulate the Motion Of A Helicoptermentioning
confidence: 99%
“…Instead, when all blades take an angle of attack α c > 0 the thrust is no longer null and the turning of the blades produces a vertical thrust that tends to counteract the helicopter's weight force. The Equation (22) becomes:…”
Section: Model Of a Helicopter With A Single Principal Rotor And A Tail Rotormentioning
confidence: 99%
“…A discrete‐time system implementing the leader gyrostat and follower gyrostat, realised by a forward Euler method with stepsize h , are laid out in the following (details on numerical integration methods on Lie groups may be found, e.g. in [19, 39]). The equations for the leader gyrostat read {right left right left right left right left right left right left0.278em 2em 0.278em 2em 0.278em 2em 0.278em 2em 0.278em 2em 0.278em.5emC k := [ κ 1 ( ω r ω x , k ) + κ 2 ( ω r 3 ω x , k 3 ) ] normalΩ x + [ κ 3 ( ω r ω y , k ) + κ 4 ( ω r 3 ω y , k 3 ) ] normalΩ y + [ κ 5 ( ω r ω z , k ) + κ 6 ( ω r 3 ω z , k 3 ) ] normalΩ z , B k := J 11 ω 1 Ω x + J 22 ω 2 Ω y + J 33 ω 3 false( 1 + b cos false( ν h k false) false) Ω z , B ˙ k := J 33 ν thinmathspaceb thinmathspaceω 3 sin false( ν h k false) Ω z , right left right left right left right left right left right left0.278em 2em 0.278em 2em 0.278em 2em 0.278em 2em 0.278em 2em 0.278em.5emW k + 1 = W k + h…”
Section: Application Of L‐pid To Time Synchronisation Of Two Physicmentioning
confidence: 99%