Note: This page has not been verified by our editors.
Description
The flexible space structure benchmark[1] is a procedural modal model which represents structural dynamics with a selectable number actuators and sensors.
Model
In modal form the flexible space structure model for modes, actuators and sensors is of second order and given by:
- Failed to parse (syntax error): {\displaystyle \ddot{\nu}(t) &= (2 \xi \circ \omega) \circ \dot{\nu}(t) + (\omega \circ \omega) \circ \nu = Bu(t) \\ y(t) &= C_r\dot{\nu}(t) + C_d\nu(t) }
with the parameters (damping ratio), (natural frequency) and using the Hadamard product $\circ$. The first order representation follows for by:
- Failed to parse (syntax error): {\displaystyle \dot{x}(t) &= Ax(t) + Bu(t) \\ y(t) &= Cx(t) }
with the matrices:
- Failed to parse (syntax error): {\displaystyle A := \begin{pmatrix} A_1 & & \\ & \ddots & \\ & & A_K \end{pmatrix}, \\ B := \begin{pmatrix} B_1 \\ \vdots \\ B_K \end{pmatrix}, \\ C := \begin{pmatrix} C_1 & \dots & C_K \end{pmatrix}, }
and their components:
- Failed to parse (syntax error): {\displaystyle A_k := \begin{pmatrix} -2\xi_k\omega_k & -\omega_k \\ \omega_k & 0 \end{pmatrix}, \\ B_k := \begin{pmatrix} b_k \\ 0 \end{pmatrix}, \\ C_k := \begin{pmatrix} c_{rk} & \frac{c_{dk}}{\omega_k} \end{pmatrix}, }
where and .
Benchmark Specifics
For this benchmark the system matrix is block diagonal and thus chosen to be sparse. The parameters and math>\omega</math> are sampled from a uniform random distributions Failed to parse (syntax error): {\displaystyle \mathcal{U}_[0,\frac{1}{1000}]}^K} and Failed to parse (syntax error): {\displaystyle \mathcal{U}_[0,100]}^K} respectively. The components of the input matrix are sampled form a uniform random distribution , while the output matrix is sampled from a uniform random distribution completely w.l.o.g, since if the components of are random their scaling can be ignored.
Data
The following Matlab code assembles the above described , and matrix for a given number of modes .
function [A,B,C] = fss(K,M,Q)
rand('seed',1009);
xi = rand(1,K)*0.001; % Sample damping ratio
omega = rand(1,K)*100; % Sample natural frequencies
A_k = cellfun(@(p) sparse([-2.0*p(1)*p(2),-p(2);p(2),0]), ...
num2cell([xi;omega],1),'UniformOutput',0);
A = blkdiag(A_k{:});
B = kron(rand(K,M),[1;0]);
C = 10.0*rand(Q,2*K);
end
Reference
- ↑ W. Gawronski and T. Williams, "Model Reduction for Flexible Space Structures", Journal of Guidance 14(1): 68--76, 1991