From 4cafd296724faa1023b289029f0fcf7ba92cce95 Mon Sep 17 00:00:00 2001 From: Nao Pross Date: Fri, 5 Apr 2024 01:30:24 +0200 Subject: Replace LQR with H-infinity design --- uav_params.m | 7 ++++--- 1 file changed, 4 insertions(+), 3 deletions(-) (limited to 'uav_params.m') 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; -- cgit v1.2.1