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-rw-r--r--uav_params.m7
1 files changed, 4 insertions, 3 deletions
diff --git a/uav_params.m b/uav_params.m
index 0e82148..7bed89c 100644
--- a/uav_params.m
+++ b/uav_params.m
@@ -1,6 +1,6 @@
-% Copyright (C) 2024, Naoki Sean Pross, ETH Zürich
+% Retrieve or compute parameters for ducted-fan VTOL micro-UAV.
%
-% Retrieve / compute parameters for UAV.
+% Copyright (C) 2024, Naoki Sean Pross, ETH Zürich
function [params] = uav_params()
@@ -48,7 +48,7 @@ params.actuators = struct(...
params.measurements = struct(...
'SensorFusionBandwidth', 1e3, ...
- 'MeasurementDelay', 8e-3 ... % delay caused by sensor fusion algorithm
+ 'SensorFusionDelay', 8e-3 ...
);
% ------------------------------------------------------------------------
@@ -73,6 +73,7 @@ params.aerodynamics = struct(...
% Compute theoretical thrust required to make the UAV hover
% from the relation mg = k * omega^2
+% FIXME: This value should probably be replaced with a measurement
g = params.physics.Gravity;
m = params.mechanical.Mass;
k = params.aerodynamics.ThrustOmegaProp;