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authorNao Pross <np@0hm.ch>2024-05-31 15:31:02 +0200
committerNao Pross <np@0hm.ch>2024-05-31 15:31:02 +0200
commitd2d174694099a2e9e88124287e2fd32c3cc4e808 (patch)
tree5bb4a53a820ec32d175845a9062888fdb26b4f96 /uav_params.m
parentAdd worst case (diff)
downloaduav-master.tar.gz
uav-master.zip
Update model and weightsHEADmaster
Diffstat (limited to '')
-rw-r--r--uav_params.m4
1 files changed, 2 insertions, 2 deletions
diff --git a/uav_params.m b/uav_params.m
index 8963b02..8c73ae9 100644
--- a/uav_params.m
+++ b/uav_params.m
@@ -88,13 +88,13 @@ 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 %
+ 'ThrustOmegaPropUncertainty', .01, ... % in %
'FlapArea', 23e-3 * 10e-3, ... % in m^2
'FlapAreaUncertainty', .1, ... % in %
'DragCoefficients', [0, 0], ... % TODO
'DragCoefficientsUncertainties', [.0, .0], ... % in %
'LiftCoefficient', 2 * pi, ... % TODO
- 'LiftCoefficientUncertainty', .05 ...% in %
+ 'LiftCoefficientUncertainty', .01 ...% in %
);