نتایج جستجو برای: inertia matrix

تعداد نتایج: 376179  

Journal: :مدیریت فرهنگ سازمانی 0
وحید خاشعی استادیار، دانشکدة مدیریت و حسابداری، دانشگاه علامه طباطبایی، تهران، ایران علی محمدی نسب کارشناس ارشد، دانشکدة مدیریت و حسابداری، دانشگاه علامه طباطبایی، تهران، ایران الهه مهدی زاده کارشناس ارشد، دانشکدة مدیریت و حسابداری، پردیس فارابی دانشگاه تهران، قم، ایران

this study aims to examine how open innovation can be effective in changing organizational inertia to create business model innovation and improve firm performance. it also seeks to explore whether the existence of open innovation has a mediating effect and influence. this study constructs a theoretical model to explore the relationship between latent variables and uses a questionnaire to colle...

2011
Lin Liao

[Abstract] Inertia relief analysis is regarded as an effective technique for the modeling of unconstrained structural systems. In this paper the principle of inertia relief analysis is first described. Inertia relief capability of commercial finite element packages is discussed. The paper studies the implementation of inertia relief techniques into finite element analysis of a variety of struct...

2014
Minyeon Han Jisoo Hong F. C. Park

Recent studies have shown that the constant inertia assumption made in typical muscle dynamic models can lead to significant discrepancies in accuracy of simulation or inverse dynamics. This paper proposes a general framework for musculoskeletal dynamic simulation that takes into account changes in muscle inertia that occur during movement. We first develop a general shape-varying muscle mass m...

Journal: :CoRR 2017
Ravi N. Banavar Arjun Narayanan

Nomenclature β,γ(∈ S) = The gimbal and wheel angles. (rad) Rβ(∈ SO(3)) = Transformation from gimbal frame G to the spacecraft body frame B. Is = Spacecraft inertia without the CMG gimbal and wheel inertia. (kg.m) Ig, Ir = Gimbal frame inertia, wheel inertia about own centre of mass represented in gimbal frame. (kg.m) (Igr)β = Combined inertia of gimbal frame and wheel in the spacecraft frame. R...

2005
K V Fernando

Recently Fernando successfully resurrected a classical method for computing eigen vectors which goes back to the times of Cauchy This algorithm has been in the doldrums for nearly fty years because of a fundamental di culty highlighted by Wilkinson The algorithm is based on the solution of a nearly homogeneous system of equations J I z k ek zk for the approximate eigenvector z where is an eigen...

2013
Ying Liu Weigen Yan Y. Liu

Let G be a graph with n vertices and ν(G) be the matching number of G. The inertia of a graph G, In(G) = (n+, n−, n0) is an integer triple specifying the numbers of positive, negative and zero eigenvalues of the adjacency matrix A(G), respectively. Let η(G) = n0 denote the nullity of G (the multiplicity of the eigenvalue zero of G). It is well known that if G is a tree, then η(G) = n− 2ν(G). Gu...

2015
Shibing Deng Shuchao Li Feifei Song

Let Gw be a weighted graph. The inertia of Gw is the triple In(Gw) = (i+(Gw), i−(Gw), i0(Gw)), where i+(Gw), i−(Gw), i0(Gw) are, respectively, the number of the positive, negative and zero eigenvalues of the adjacency matrix A(Gw) of Gw including their multiplicities. A simple n-vertex connected graph is called a (k − 1)-cyclic graph if its number of edges equals n + k − 2. Let θ(r1, r2, . . . ...

2003
Chi-Kwong Li Nung-Sing Sze Yung-Chow Wong

Let H1 be an n × n invertible Hermitian matrix, and let U(H1) be the group of n × n H1-unitary matrices, i.e., matrices A satisfying A H1A = H1. Suppose H2 is an m × m invertible Hermitian matrix. We show that a linear transformation φ : Mn → Mm satisfies φ(U(H1)) ⊆ U(H2) if and only if there exist invertible matrices S ∈ Mm, U, V ∈ U(H2) such that SH2S = [(Ia ⊕−Ib)⊗H1]⊕ [(Ic ⊕−Id)⊗ (H−1 1 )], ...

2015
Gongliu Yang Yuanyuan Liu Ming Li Shunguang Song

An improved double-factor adaptive Kalman filter called AMA-RWE-DFAKF is proposed to denoise fiber optic gyroscope (FOG) drift signal in both static and dynamic conditions. The first factor is Kalman gain updated by random weighting estimation (RWE) of the covariance matrix of innovation sequence at any time to ensure the lowest noise level of output, but the inertia of KF response increases in...

2000
Yixin Chen John E. McInroy

By exploiting properties of the joint space mass-inertia matrix of flexure jointed hexapods, a new decoupling method is proposed. The new decoupling method, through a static input-output mapping, transforms the highly coupled 6 input 6 output dynamics into 6 independent single-input single-output (SISO) channels. Controls for these SISO channels are far simpler than their multiple-input multipl...

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