plot_CGloc {AvInertia} | R Documentation |
Plot the center of gravity of each component
Description
Plot the center of gravity of each component
Usage
plot_CGloc(
clean_pts,
mass_properties,
mass_properties_skin,
mass_properties_bone,
mass_properties_feathers,
mass_properties_muscle,
prop_tertiary1,
prop_tertiary2,
plot_var
)
Arguments
clean_pts |
Dataframe of the key positions of the bird as follows:
|
mass_properties |
Dataframe containing the center of gravity and moment of inertia components of the full wing. |
mass_properties_skin |
Dataframe containing the center of gravity and moment of inertia components of the skin. Formatted with the following columns: "species","BirdID","TestID","FrameID", "prop_type","component","value". |
mass_properties_bone |
Dataframe containing the center of gravity and moment of inertia components of the wing bones. Formatted with the following columns: "species","BirdID","TestID","FrameID", "prop_type","component","value". |
mass_properties_feathers |
Dataframe containing the center of gravity and moment of inertia components of the feathers. Formatted with the following columns: "species","BirdID","TestID","FrameID", "prop_type","component","value". |
mass_properties_muscle |
Dataframe containing the center of gravity and moment of inertia components of the muscles Formatted with the following columns: "species","BirdID","TestID","FrameID", "prop_type","component","value". |
prop_tertiary1 |
Dataframe containing the center of gravity and moment of inertia components of the first tertiary group. Formatted with the following columns: "species","BirdID","TestID","FrameID", "prop_type","component","value". |
prop_tertiary2 |
Dataframe containing the center of gravity and moment of inertia components of the second tertiary group. Formatted with the following columns: "species","BirdID","TestID","FrameID", "prop_type","component","value". |
plot_var |
Character of either "yx" or "yz". Defines the output axes of the plot. |
Value
A plot of the request axes
Examples
# refer to the vignette
library(AvInertia)
# load data
data(dat_id_curr, package = "AvInertia")
data(dat_bird_curr, package = "AvInertia")
data(dat_feat_curr, package = "AvInertia")
data(dat_bone_curr, package = "AvInertia")
data(dat_mat, package = "AvInertia")
data(clean_pts, package = "AvInertia")
# 1. Determine the center of gravity of the bird's torso (including the legs)
dat_torsotail_out = massprop_restbody(dat_id_curr, dat_bird_curr)
# 2. Calculate the inertia of the flight feathers about the tip of the calamus
feather_inertia <- compute_feat_inertia(dat_mat, dat_feat_curr, dat_bird_curr)
# 3. Determine the center of gravity of one of the bird's wings
dat_wing_out = massprop_birdwing(dat_id_curr, dat_bird_curr,
dat_bone_curr, dat_feat_curr, dat_mat, clean_pts,
feather_inertia, plot_var = 0)
# Visualize the center of gravity of each wing component in the x and y axis
dat_wing_out = massprop_birdwing(dat_id_curr, dat_bird_curr,
dat_bone_curr, dat_feat_curr, dat_mat, clean_pts,
feather_inertia, plot_var = "yx")
# or the y and z axis
dat_wing_out = massprop_birdwing(dat_id_curr, dat_bird_curr,
dat_bone_curr, dat_feat_curr, dat_mat, clean_pts,
feather_inertia, plot_var = "yz")
# 4. Combine all data and obtain the center of gravity, moment of inertia
# and principal axes of the bird
curr_full_bird = combine_inertialprop(dat_torsotail_out,dat_wing_out,
dat_wing_out, dat_id_curr, dat_bird_curr, symmetric=TRUE)