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-rw-r--r--uav_params.m16
1 files changed, 8 insertions, 8 deletions
diff --git a/uav_params.m b/uav_params.m
index e87e4fd..fdd519a 100644
--- a/uav_params.m
+++ b/uav_params.m
@@ -40,7 +40,7 @@ r_prop = 85e-3; % radius of propeller
J_prop = .5 * m_prop * r_prop^2;
params.mechanical = struct(...
- 'Mass', 3.0, ...
+ 'Mass', 3.5, ...
'DuctRadius', 46e-3, ...
'DuctHeight', 171e-3, ...
'FlapZDistance', 98e-3, ... % flap distance along z from center of mass
@@ -65,7 +65,7 @@ params.actuators = struct(...
% IMU runs in NDOF mode
params.measurements = struct(...
- 'SensorFusionDelay', 50e-3, ... % in s
+ 'SensorFusionDelay', 30e-3, ... % in s
'LIDARAccuracy', 10e-3, ... % in m
'LIDARMaxDistance', 40, ... % inm
'LIDARBandwidth', 100, ... % in Hz for z position
@@ -91,13 +91,13 @@ 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', .01, ... % in %
- 'DragCoefficients', [1, .1], ... % TODO
+ 'FlapAreaUncertainty', .02, ... % in %
+ 'DragCoefficients', [0, 0], ... % TODO
'DragCoefficientsUncertainties', [.1, .1], ... % in %
'LiftCoefficient', 2 * pi, ... % TODO
- 'LiftCoefficientUncertainty', .1 ...% in %
+ 'LiftCoefficientUncertainty', .05 ...% in %
);
@@ -114,7 +114,7 @@ k = params.aerodynamics.ThrustOmegaProp;
omega_hover = sqrt(m * g / k);
params.linearization = struct(...
- 'PadeApproxOrder', 2, ...
+ 'PadeApproxOrder', 3, ...
'Position', [0; 0; -2], ... % in inertial frame, z points down
'Velocity', [0; 0; 0], ... % in inertial frame
'Angles', [0; 0; pi / 4], ... % in body frame
@@ -123,7 +123,7 @@ params.linearization = struct(...
);
% ------------------------------------------------------------------------
-% Performance requirements
+% Normalization (maximum values)
params.normalization = struct(...
'HPosition', 1, ... % m