diff options
Diffstat (limited to 'uav_params.m')
| -rw-r--r-- | uav_params.m | 10 |
1 files changed, 8 insertions, 2 deletions
diff --git a/uav_params.m b/uav_params.m index da8a19b..a1c0e4a 100644 --- a/uav_params.m +++ b/uav_params.m @@ -11,6 +11,7 @@ function [params] = uav_params() % Time in s % Frequencies in Hz % Angular velocities in rad / s +% Uncertainty / measurement errors in percentage (between 0 and 1) params = struct(); @@ -44,7 +45,8 @@ params.mechanical = struct(... 'DuctHeight', 171e-3, ... 'FlapZDistance', 98e-3, ... % flap distance along z from center of mass 'InertiaTensor', J, ... - 'GyroscopicInertiaZ', J_prop ... % assume small angle + 'GyroscopicInertiaZ', J_prop, ... % assume small angle + 'GyroscopicInertiaZUncertainty', .01 ... % in % ); % ------------------------------------------------------------------------ @@ -84,9 +86,13 @@ k_T = F_max / omega_max^2; % https://scienceworld.wolfram.com/physics/LiftCoefficient.html params.aerodynamics = struct(... 'ThrustOmegaProp', k_T, ... % in s^2 / (rad * N) + 'ThrustOmegaPropUncertainty', .05, ... % in % 'FlapArea', 23e-3 * 10e-3, ... % in m^2 + 'FlapAreaUncertainty', .01, ... % in % 'DragCoefficients', [1, .1], ... % TODO - 'LiftCoefficient', 2 * pi ... % TODO + 'DragCoefficientsUncertainties', [.1, .1], ... % in % + 'LiftCoefficient', 2 * pi, ... % TODO + 'LiftCoefficientUncertainty', .1 ...% in % ); |