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ISS SPHERES

Code(Git)

ISS SPHERES Code(Git)

SPHERES Facility software for scientists

Status: Alpha
Brought to you by: alvarso, danroa, dmiller7115, jvbenavi, sphereseng

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[66ae6b]: / SSSM / plot_sssm_results.m  Maximize  Restore  History

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%% PLOT OF SIMULATION RESULTS

% This portion of the software is responsible for plotting position and

% associated velocity/angular velocity components of the SPHERES set-up.

%%

% Plot of [x, y, z] positions and [Xdot, Ydot, Zdot] velocity components

figure,

subplot(3,2,1), plot(state.time,state.signals.values(:,1),'r','LineWidth',3),

grid on, xlabel('time[s]'), ylabel('x[m/s]'),title('x position comparison'),

xlim([0 state.time(end,:)])

subplot(3,2,2), plot(state.time,state.signals.values(:,4),'r','LineWidth',3),

grid on, xlabel('time[s]'), ylabel('xdot[m/s^2]'),title('x velocity comparison'),

xlim([0 state.time(end,:)])

subplot(3,2,3), plot(state.time,state.signals.values(:,2),'r','LineWidth',3),

grid on, xlabel('time[s]'), ylabel('y[m/s]'),title('y position comparison'),

xlim([0 state.time(end,:)])

subplot(3,2,4), plot(state.time,state.signals.values(:,5),'r','LineWidth',3),

grid on, xlabel('time[s]'), ylabel('ydot[m/s^2]'),title('y velocity comparison'),

xlim([0 state.time(end,:)])

subplot(3,2,5), plot(state.time,state.signals.values(:,3),'r','LineWidth',3),

grid on, xlabel('time[s]'), ylabel('z[m/s]'),title('z position comparison'),

xlim([0 state.time(end,:)])

subplot(3,2,6), plot(state.time,state.signals.values(:,6),'r','LineWidth',3),

grid on, xlabel('time[s]'), ylabel('zdot[m/s^2]'),title('z velocity comparison'),

xlim([0 state.time(end,:)])

%%

% Plot of Thruster Vector Dynamics (i.e. thruster firings):

figure,

subplot(3,4,1),

plot(ThrustVectorOutputs.time,...

ThrustVectorOutputs.signals.values(:,1),...

'b','LineWidth',3)

grid on, xlabel('time[s]'), ylabel('On / Off'),title('Thruster-01'),

xlim([0 state.time(end,:)])

subplot(3,4,2),

plot(ThrustVectorOutputs.time,...

ThrustVectorOutputs.signals.values(:,2),...

'b','LineWidth',3)

grid on, xlabel('time[s]'), ylabel('On / Off'),title('Thruster-02'),

xlim([0 state.time(end,:)])

subplot(3,4,3),

plot(ThrustVectorOutputs.time,...

ThrustVectorOutputs.signals.values(:,3),...

'b','LineWidth',3)

grid on, xlabel('time[s]'), ylabel('On / Off'),title('Thruster-03'),

xlim([0 state.time(end,:)])

subplot(3,4,4),

plot(ThrustVectorOutputs.time,...

ThrustVectorOutputs.signals.values(:,4),...

'b','LineWidth',3)

grid on, xlabel('time[s]'), ylabel('On / Off'),title('Thruster-04'),

xlim([0 state.time(end,:)])

subplot(3,4,5),

plot(ThrustVectorOutputs.time,...

ThrustVectorOutputs.signals.values(:,5),...

'b','LineWidth',3)

grid on, xlabel('time[s]'), ylabel('On / Off'),title('Thruster-05'),

xlim([0 state.time(end,:)])

subplot(3,4,6),

plot(ThrustVectorOutputs.time,...

ThrustVectorOutputs.signals.values(:,6),...

'b','LineWidth',3)

grid on, xlabel('time[s]'), ylabel('On / Off'),title('Thruster-06'),

xlim([0 state.time(end,:)])

subplot(3,4,7),

plot(ThrustVectorOutputs.time,...

ThrustVectorOutputs.signals.values(:,7),...

'b','LineWidth',3)

grid on, xlabel('time[s]'), ylabel('On / Off'),title('Thruster-07'),

xlim([0 state.time(end,:)])

subplot(3,4,8),

plot(ThrustVectorOutputs.time,...

ThrustVectorOutputs.signals.values(:,8),...

'b','LineWidth',3)

grid on, xlabel('time[s]'), ylabel('On / Off'),title('Thruster-08'),

xlim([0 state.time(end,:)])

subplot(3,4,9),

plot(ThrustVectorOutputs.time,...

ThrustVectorOutputs.signals.values(:,9),...

'b','LineWidth',3)

grid on, xlabel('time[s]'), ylabel('On / Off'),title('Thruster-09'),

xlim([0 state.time(end,:)])

subplot(3,4,10),

plot(ThrustVectorOutputs.time,...

ThrustVectorOutputs.signals.values(:,10),...

'b','LineWidth',3)

grid on, xlabel('time[s]'), ylabel('On / Off'),title('Thruster-010'),

xlim([0 state.time(end,:)])

subplot(3,4,11),

plot(ThrustVectorOutputs.time,...

ThrustVectorOutputs.signals.values(:,11),...

'b','LineWidth',3)

grid on, xlabel('time[s]'), ylabel('On / Off'),title('Thruster-010'),

xlim([0 state.time(end,:)])

subplot(3,4,12),

plot(ThrustVectorOutputs.time,...

ThrustVectorOutputs.signals.values(:,12),...

'b','LineWidth',3)

grid on, xlabel('time[s]'), ylabel('On / Off'),title('Thruster-012'),

xlim([0 state.time(end,:)])

%%

% Copyright (c) 2015, San Jose State Universtity Control Science & Dynamical Systems (CSDy) Laboratory

% All rights reserved.

%

% Redistribution and use in source and binary forms, with or without modification, are permitted

% provided that the following conditions are met:

% Redistributions of source code must retain the above copyright notice, this list of conditions and

% the following disclaimer.

% Redistributions in binary form must reproduce the above copyright notice, this list of conditions and

% the following disclaimer in the documentation and/or other materials provided with the distribution.

% Neither the name of the Massachusetts Institute of Technology, the MIT Space Systems Laboratory, nor

% the names of its contributors may be used to endorse or promote products derived from this software

% without specific prior written permission.

%

% THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS "AS IS" AND ANY EXPRESS OR

% IMPLIED WARRANTIES, INCLUDING, BUT NOT LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND

% FITNESS FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE COPYRIGHT HOLDER OR

% CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL

% DAMAGES (INCLUDING, BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS OF USE,

% DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED AND ON ANY THEORY OF LIABILITY,

% WHETHER IN CONTRACT, STRICT LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN

%

% ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE POSSIBILITY OF SUCH DAMAGE.

%

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