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Inferring flight parameters of Mesozoic avians through multivariate analyses of forelimb elements in their living relatives

Published online by Cambridge University Press:  06 December 2016

Francisco J. Serrano
Affiliation:
Departamento de Ecología y Geología, Facultad de Ciencias, Universidad de Málaga. Campus Universitario de Teatinos s/n, 29071 Málaga, Spain. E-mail: fjsa@uma.es, ppb@uma.es.
Paul Palmqvist
Affiliation:
Departamento de Ecología y Geología, Facultad de Ciencias, Universidad de Málaga. Campus Universitario de Teatinos s/n, 29071 Málaga, Spain. E-mail: fjsa@uma.es, ppb@uma.es.
Luis M. Chiappe
Affiliation:
Dinosaur Institute, Natural History Museum of Los Angeles County, 900 Exposition Boulevard, Los Angeles, California 90007, U.S.A. E-mail: lchiappe@nhm.org
José L. Sanz
Affiliation:
Unidad de Paleontología, Departamento de Biología, Facultad de Ciencias, Universidad Autónoma de Madrid, Calle Darwin 2, Cantoblanco, 28049 Madrid, Spain. E-mail: dinoproyecto@gmail.com

Abstract

Our knowledge of the diversity, ecology, and phylogeny of Mesozoic birds has increased significantly during recent decades, yet our understanding of their flight competence remains poor. Wing loading (WL) and aspect ratio (AR) are two aerodynamically relevant parameters, as they relate to energy costs of aerial locomotion and flight maneuverability. They can be calculated in living birds (i.e., Neornithes) from body mass (BM), wingspan (B), and lift surface (S L). However, the estimates for extinct birds can be subject to biases from statistical issues, phylogeny, locomotor adaptations, and diagenetic compaction. Here we develop a sequential approach for generating reliable multivariate models that allow estimation of measurements necessary to determine WL and AR in the main clades of non-neornithine Mesozoic birds. The strength of our predictions is supported by the use of those variables that show similar scaling patterns in modern and stem taxa (i.e., non-neornithine birds) and the similarity of our predictions with measurements obtained from fossils preserving wing outlines. In addition, although our WL and AR values are based on estimates (BM, B, and S L) that have an associated error, there is no cumulative error in their calculation, and both parameters show low prediction errors. Therefore, we present the first taxonomically broad, error-calibrated estimation of these two important aerodynamic parameters in non-neornithine birds. Such estimates show that the WL and AR of the non-neornithine birds here analyzed fall within the range of variation of modern birds (i.e., Neornithes). Our results indicate that most modern flight modes (e.g., continuous flapping, flap and gliding, flap and bounding, thermal soaring) were possible for the wide range of non-neornithine avian taxa; we found no evidence for the presence of dynamic soaring among these early birds.

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Copyright © 2016 The Paleontological Society. All rights reserved 
Figure 0

Figure 1 Measurements of wing elements used in this study (defined in Table 1). A, Skeletal forelimb elements: humerus (cranial aspect), ulna (dorsal aspect), radius (dorsal aspect), and carpometacarpus (dorsal aspect). B, Bird silhouette for illustrating the furcula and feathered wing measurements.

Figure 1

Table 1 Definition of measurements of the forelimb elements used in this study, which are illustrated in Fig. 1.

Figure 2

Table 2 Ordinary least-squares (OLS) single regressions (SR) with the best-correlated x variables (*; i.e., higher Pearson coefficient), the best multiple regressions (MR), and the principal component regressions (PCR), derived to predict B and SL. N, number of individuals; R2adj, coefficient of determination adjusted for the number of predictors included in the model; |%MPE|, mean percentage prediction error calculated over the whole data set; |%MPE|VS-25%, mean percentage prediction error calculated over the validating subsample of 25% species from the data set; |%MPE|VS-GA, mean percentage prediction error calculated using Galloansarae as validating subsample; VIF, variance inflation factor, 1/(1−R2).

Figure 3

Table 3 Effects of the taxonomic weighting and the stepwise procedure on the prediction errors of the best MRs derived from the modern bird data set. |%MPE|, mean percentage prediction error calculated over the whole data set; |%MPE|VS-25%, mean percentage prediction error calculated over the validating subsample of 25% species from the data set; |%MPE|VS-GA, mean percentage prediction error calculated using Galloansarae as validating subsample. Asterisk (*) indicates that the stepwise procedure extracted the same function as the full model.

Figure 4

Table 4 OLS single regressions obtained for each predictor variable against wingspan (B), using the means of species calculated from raw data and the appropriate phylogenetically independent contrasts (PICs). PICs assume a regression through the origin (a=0). Statistical significance of the regressions was checked by permutation tests with 10,000 replicates and 95% bootstrapped confidence intervals of the slopes (CI) are also shown. Slope difference significance between OLS raw data and OLS PICs were tested using Student’s t-test (α=0.05). For abbreviations of variables, see Table 1.

Figure 5

Table 5 OLS single regressions obtained for each predictor variable against wing area (SL), using the means of species calculated from raw data and the appropriate PICs. PICs assume a regression through the origin (a=0). Statistical significance of the regressions was checked by permutation tests with 10,000 replicates and 95% bootstrapped confidence intervals of the slopes (CI) are also shown. Slope difference significance between OLS raw data and OLS PICs were tested using Student’s t-test (α=0.05). For abbreviations of variables, see Table 1.

Figure 6

Figure 2 Relationship between interclavicular distance (WF) and a proxy of wingspan, Lw* (taken as the cumulative length of HL, UL, CmL, LDII, and Lprim) in modern flying birds and those stem birds in which these variables could be unequivocally measured. The gray line corresponds to the RMA slope for Neognathae (log WF=1.142 log Lw* −1.555; N=326). The black line represents the RMA slope for stem birds (log WF=1.178 log Lw* −1.607; N=10). R2 and the p-values of the regressions (obtained with permutation test with 10,000 replicates) are displayed in the graph.

Figure 7

Figure 3 Proportion between the longest primary feather (Lprim) and the length of the wing skeleton (Lwsk) in the main avian taxa. Abbreviations: Arch, Archaeopterygidae; Jeh, Jeholornithidae; Sape, Sapeornithidae; Conf, Confuciusornithidae; Enan, Enantiornithes; Orph, basal members of Ornithuromorpha; Neo, Neognathae. Box length in neognaths indicates the interquartile range (25th and 75th percentiles) and horizontal lines show the 5–95% confidence limits. Black points are outliers.

Figure 8

Table 6 OLS MRs derived for predicting wingspan (B) in avian taxa. For abbreviations of variables, see Table 1. N, number of individuals; R2adj, coefficient of determination adjusted for the number of predictors included in the model; |%MPE|, mean percent prediction error calculated over the whole data set; |%MPE|VS-25%, mean percent prediction error calculated over the validating subsample (25% species); |%MPE|VS-GA=mean percentage prediction error calculated using Galloanserae as validating subsample.

Figure 9

Figure 4 Scaling of the anatomical variables against estimated wing surface (SL) in modern and stem birds. The biplots are used in the procedure of selection of variables for each basal group of Mesozoic birds (identified with different symbols). Each of 16 anatomical variables was plotted against a combination of the remaining variables used for estimating SL (Table 7). Each biplot shows the OLS regression line fitted for extant birds (gray circles) with the 95% confidence intervals for SL predictions (dotted lines), the R2 value, and the p-value of the regression (obtained with permutation test with 10,000 replicates).

Figure 10

Table 7 OLS MRs used in the procedure for selection of variables. Three functions to predict SL were obtained from different combinations of the anatomical predictors (MR Sel.1-3). The SL values obtained in these functions were plotted against each predictor variable to test and select those for specific stem taxa (Fig. 4 and Table 8).

Figure 11

Table 8 Forelimb variables discarded after the selection procedure for predicting SL on each avian taxa.

Figure 12

Table 9 OLS MRs obtained for predicting wing area (SL) in each avian taxon. For abbreviations of variables, see Table 1. For abbreviations of fossil taxa, see legend of Fig. 3. N, number of individuals; R2adj, coefficient of determination adjusted for the number of predictors included in the model; |%MPE|, mean percent prediction error calculated over the whole data set; |%MPE|VS-25%, mean percent prediction error calculated over the validating subsample (25% species); |%MPE|VS-GA, mean percentage prediction error calculated using Galloanserae as validating subsample.

Figure 13

Table 10 Effect of different aerial locomotion on the mean prediction error (%PE) values of the best SR equation and the MR models obtained. Flying mode abbreviations: CF, continuous flapping; FG, flap and gliding; FB, flap and bounding; S, soaring. For abbreviations of variables, see Table 1. When Levene’s test (Lev.) was nonsignificant, the difference between groups was tested by a one-way ANOVA. In other cases, Welch’s test was performed. For abbreviations of fossil taxa, see legend of Fig.3.

Figure 14

Table 11 Calibration of the cumulative prediction error on flight parameters.

Figure 15

Table 12 Estimates of the basic and compound variables for the specimens of Mesozoic stem taxa. The multiple regression model from which wingspan (B) and wing area (SL) were obtained, are also indicated (MR-B and MR-SL, from Tables 6 and 9). The body mass values (BM) obtained in Serrano et al. (2015) are also included for a summary. The prediction errors (%MPEs) of wing loading (WL) and aspect ratio (AR) calculated on the modern data set are also shown for different combinations of B, SL, and BM estimates. Prediction intervals were calculated as predicted values ± |%MPE| values.

Figure 16

Table 13 Comparison between the estimates for Berlin’s Archaeopteryx and for Hongshanornis (two specimens) obtained using MR models (first line of each taxon) and outline body reconstructions. Superscript numbers indicate the method for obtaining BM values used in each study. The difference (in percent variation) between estimates from published reconstructions and estimates obtained in the present work is also shown.

Figure 17

Figure 5 Range of values for the aerodynamic variables calculated in the present study for stem avian taxa and flying neognaths. Modern birds are distributed according to their predominant flight mode. Each box plot represents one stem taxon or modern flight mode. Box length shows the interquartile range (25th and 75th percentiles). Whisker lengths indicate the 5–95% confidence limits. Unfilled circles represents individuals out of this range, and asterisks indicate outliers. A, Wing-loading values. B, Aspect ratio values.