#+TITLE: Stewart Platform - Dynamics Study :DRAWER: #+HTML_LINK_HOME: ./index.html #+HTML_LINK_UP: ./index.html #+HTML_HEAD: #+HTML_HEAD: #+HTML_HEAD: #+HTML_HEAD: #+HTML_HEAD: #+HTML_HEAD: #+PROPERTY: header-args:matlab :session *MATLAB* #+PROPERTY: header-args:matlab+ :comments org #+PROPERTY: header-args:matlab+ :exports both #+PROPERTY: header-args:matlab+ :results none #+PROPERTY: header-args:matlab+ :eval no-export #+PROPERTY: header-args:matlab+ :noweb yes #+PROPERTY: header-args:matlab+ :mkdirp yes #+PROPERTY: header-args:matlab+ :output-dir figs :END: * Some tests ** Matlab Init :noexport:ignore: #+begin_src matlab :tangle no :exports none :results silent :noweb yes :var current_dir=(file-name-directory buffer-file-name) <> #+end_src #+begin_src matlab :exports none :results silent :noweb yes <> #+end_src #+begin_src matlab simulinkproject('./'); #+end_src ** Simscape Model #+begin_src matlab open('stewart_platform_dynamics.slx') #+end_src ** test #+begin_src matlab stewart = initializeFramesPositions(); stewart = generateGeneralConfiguration(stewart); stewart = computeJointsPose(stewart); stewart = initializeStrutDynamics(stewart); stewart = initializeCylindricalPlatforms(stewart); stewart = initializeCylindricalStruts(stewart); stewart = computeJacobian(stewart); stewart = initializeStewartPose(stewart); #+end_src Estimation of the transfer function from $\mathcal{\bm{F}}$ to $\mathcal{\bm{X}}$: #+begin_src matlab %% Options for Linearized options = linearizeOptions; options.SampleTime = 0; %% Name of the Simulink File mdl = 'stewart_platform_dynamics'; %% Input/Output definition clear io; io_i = 1; io(io_i) = linio([mdl, '/F'], 1, 'openinput'); io_i = io_i + 1; io(io_i) = linio([mdl, '/X'], 1, 'openoutput'); io_i = io_i + 1; %% Run the linearization G = linearize(mdl, io, options); G.InputName = {'Fx', 'Fy', 'Fz', 'Mx', 'My', 'Mz'}; G.OutputName = {'Edx', 'Edy', 'Edz', 'Erx', 'Ery', 'Erz'}; #+end_src #+begin_src matlab %% Options for Linearized options = linearizeOptions; options.SampleTime = 0; %% Name of the Simulink File mdl = 'stewart_platform_dynamics'; %% Input/Output definition clear io; io_i = 1; io(io_i) = linio([mdl, '/J-T'], 1, 'openinput'); io_i = io_i + 1; io(io_i) = linio([mdl, '/X'], 1, 'openoutput'); io_i = io_i + 1; %% Run the linearization G = linearize(mdl, io, options); G.InputName = {'F1', 'F2', 'F3', 'F4', 'F5', 'F6'}; G.OutputName = {'Edx', 'Edy', 'Edz', 'Erx', 'Ery', 'Erz'}; #+end_src #+begin_src matlab G_cart = minreal(G*inv(stewart.J')); G_cart.InputName = {'Fnx', 'Fny', 'Fnz', 'Mnx', 'Mny', 'Mnz'}; #+end_src #+begin_src matlab figure; bode(G, G_cart) #+end_src #+begin_src matlab %% Options for Linearized options = linearizeOptions; options.SampleTime = 0; %% Name of the Simulink File mdl = 'stewart_platform_dynamics'; %% Input/Output definition clear io; io_i = 1; io(io_i) = linio([mdl, '/Fext'], 1, 'openinput'); io_i = io_i + 1; io(io_i) = linio([mdl, '/X'], 1, 'openoutput'); io_i = io_i + 1; %% Run the linearization Gd = linearize(mdl, io, options); Gd.InputName = {'Fex', 'Fey', 'Fez', 'Mex', 'Mey', 'Mez'}; Gd.OutputName = {'Edx', 'Edy', 'Edz', 'Erx', 'Ery', 'Erz'}; #+end_src #+begin_src matlab freqs = logspace(0, 3, 1000); figure; bode(Gd, G) #+end_src ** Compare external forces and forces applied by the actuators Initialization of the Stewart platform. #+begin_src matlab stewart = initializeFramesPositions(); stewart = generateGeneralConfiguration(stewart); stewart = computeJointsPose(stewart); stewart = initializeStrutDynamics(stewart); stewart = initializeCylindricalPlatforms(stewart); stewart = initializeCylindricalStruts(stewart); stewart = computeJacobian(stewart); stewart = initializeStewartPose(stewart); #+end_src Estimation of the transfer function from $\mathcal{\bm{F}}$ to $\mathcal{\bm{X}}$: #+begin_src matlab %% Options for Linearized options = linearizeOptions; options.SampleTime = 0; %% Name of the Simulink File mdl = 'stewart_platform_dynamics'; %% Input/Output definition clear io; io_i = 1; io(io_i) = linio([mdl, '/F'], 1, 'openinput'); io_i = io_i + 1; io(io_i) = linio([mdl, '/X'], 1, 'openoutput'); io_i = io_i + 1; %% Run the linearization G = linearize(mdl, io, options); G.InputName = {'Fx', 'Fy', 'Fz', 'Mx', 'My', 'Mz'}; G.OutputName = {'Edx', 'Edy', 'Edz', 'Erx', 'Ery', 'Erz'}; #+end_src Estimation of the transfer function from $\mathcal{\bm{F}}_{d}$ to $\mathcal{\bm{X}}$: #+begin_src matlab %% Options for Linearized options = linearizeOptions; options.SampleTime = 0; %% Name of the Simulink File mdl = 'stewart_platform_dynamics'; %% Input/Output definition clear io; io_i = 1; io(io_i) = linio([mdl, '/Fext'], 1, 'openinput'); io_i = io_i + 1; io(io_i) = linio([mdl, '/X'], 1, 'openoutput'); io_i = io_i + 1; %% Run the linearization Gd = linearize(mdl, io, options); Gd.InputName = {'Fex', 'Fey', 'Fez', 'Mex', 'Mey', 'Mez'}; Gd.OutputName = {'Edx', 'Edy', 'Edz', 'Erx', 'Ery', 'Erz'}; #+end_src Comparison of the two transfer function matrices. #+begin_src matlab freqs = logspace(0, 4, 1000); figure; bode(Gd, G, freqs) #+end_src #+begin_important Seems quite similar. #+end_important ** Comparison of the static transfer function and the Compliance matrix Initialization of the Stewart platform. #+begin_src matlab stewart = initializeFramesPositions(); stewart = generateGeneralConfiguration(stewart); stewart = computeJointsPose(stewart); stewart = initializeStrutDynamics(stewart); stewart = initializeCylindricalPlatforms(stewart); stewart = initializeCylindricalStruts(stewart); stewart = computeJacobian(stewart); stewart = initializeStewartPose(stewart); #+end_src Estimation of the transfer function from $\mathcal{\bm{F}}$ to $\mathcal{\bm{X}}$: #+begin_src matlab %% Options for Linearized options = linearizeOptions; options.SampleTime = 0; %% Name of the Simulink File mdl = 'stewart_platform_dynamics'; %% Input/Output definition clear io; io_i = 1; io(io_i) = linio([mdl, '/F'], 1, 'openinput'); io_i = io_i + 1; io(io_i) = linio([mdl, '/X'], 1, 'openoutput'); io_i = io_i + 1; %% Run the linearization G = linearize(mdl, io, options); G.InputName = {'Fx', 'Fy', 'Fz', 'Mx', 'My', 'Mz'}; G.OutputName = {'Edx', 'Edy', 'Edz', 'Erx', 'Ery', 'Erz'}; #+end_src Let's first look at the low frequency transfer function matrix from $\mathcal{\bm{F}}$ to $\mathcal{\bm{X}}$. #+begin_src matlab :exports results :results value table replace :tangle no data2orgtable(real(freqresp(G, 0.1)), {}, {}, ' %.1e '); #+end_src #+RESULTS: | 2.0e-06 | -9.1e-19 | -5.3e-12 | 7.3e-18 | 1.7e-05 | 1.3e-18 | | -1.7e-18 | 2.0e-06 | 8.6e-19 | -1.7e-05 | -1.5e-17 | 6.7e-12 | | 3.6e-13 | 3.2e-19 | 5.0e-07 | -2.5e-18 | 8.1e-12 | -1.5e-19 | | 1.0e-17 | -1.7e-05 | -5.0e-18 | 1.9e-04 | 9.1e-17 | -3.5e-11 | | 1.7e-05 | -6.9e-19 | -5.3e-11 | 6.9e-18 | 1.9e-04 | 4.8e-18 | | -3.5e-18 | -4.5e-12 | 1.5e-18 | 7.1e-11 | -3.4e-17 | 4.6e-05 | And now at the Compliance matrix. #+begin_src matlab :exports results :results value table replace :tangle no data2orgtable(stewart.C, {}, {}, ' %.1e '); #+end_src #+RESULTS: | 2.0e-06 | 2.9e-22 | 2.8e-22 | -3.2e-21 | 1.7e-05 | 1.5e-37 | | -2.1e-22 | 2.0e-06 | -1.8e-23 | -1.7e-05 | -2.3e-21 | 1.1e-22 | | 3.1e-22 | -1.6e-23 | 5.0e-07 | 1.7e-22 | 2.2e-21 | -8.1e-39 | | 2.1e-21 | -1.7e-05 | 2.0e-22 | 1.9e-04 | 2.3e-20 | -8.7e-21 | | 1.7e-05 | 2.5e-21 | 2.0e-21 | -2.8e-20 | 1.9e-04 | 1.3e-36 | | 3.7e-23 | 3.1e-22 | -6.0e-39 | -1.0e-20 | 3.1e-22 | 4.6e-05 | #+begin_important The low frequency transfer function matrix from $\mathcal{\bm{F}}$ to $\mathcal{\bm{X}}$ corresponds to the compliance matrix of the Stewart platform. #+end_important ** Transfer function from forces applied in the legs to the displacement of the legs Initialization of the Stewart platform. #+begin_src matlab stewart = initializeFramesPositions(); stewart = generateGeneralConfiguration(stewart); stewart = computeJointsPose(stewart); stewart = initializeStrutDynamics(stewart); stewart = initializeCylindricalPlatforms(stewart); stewart = initializeCylindricalStruts(stewart); stewart = computeJacobian(stewart); stewart = initializeStewartPose(stewart); #+end_src Estimation of the transfer function from $\bm{\tau}$ to $\bm{L}$: #+begin_src matlab %% Options for Linearized options = linearizeOptions; options.SampleTime = 0; %% Name of the Simulink File mdl = 'stewart_platform_dynamics'; %% Input/Output definition clear io; io_i = 1; io(io_i) = linio([mdl, '/J-T'], 1, 'openinput'); io_i = io_i + 1; io(io_i) = linio([mdl, '/L'], 1, 'openoutput'); io_i = io_i + 1; %% Run the linearization G = linearize(mdl, io, options); G.InputName = {'F1', 'F2', 'F3', 'F4', 'F5', 'F6'}; G.OutputName = {'L1', 'L2', 'L3', 'L4', 'L5', 'L6'}; #+end_src #+begin_src matlab freqs = logspace(1, 3, 1000); figure; bode(G, 2*pi*freqs) #+end_src #+begin_src matlab bodeFig({G(1,1), G(1,2)}, freqs, struct('phase', true)); #+end_src