112 IEEE GEOSCIENCE AND REMOTE SENSING LETTERS, VOL. 12, NO. 1, JANUARY 2015
Aircraft Recognition in High-Resolution Optical
Satellite Remote Sensing Images
Qichang Wu, Hao Sun, Xian Sun, Daobing Zhang, Kun Fu, and Hongqi Wang
Abstract—Automatic aircraft recognition is a challenging task.
Conventional methods always extract the overall shapes of aircraft
at first and then represent the aircraft based on the extracted
shape with different features for recognition. The major problem
of these methods is that they have a high requirement on shape
extraction, which is too idealistic for targets in satellite images. In
this letter, we propose a new aircraft recognition approach that can
recognize aircraft robustly without perfect extraction of silhouette
or shape of aircraft as a precondition, and can deal with the
situation of parts missing and shadow disturbance. Specifically, a
direction estimation method is proposed first to align aircraft to a
same direction. Then, a reconstruction-based similarity measure
is proposed, which transforms the type recognition problem into
a reconstruction problem. Finally, a jigsaw matching pursuit al-
gorithm is proposed to solve the reconstruction problem. We use
panchromatic Quickbird imagery for evaluation, and the experi-
mental results illuminate that the proposed method is effective and
accurate.
Index Terms—Aircraft recognition, image processing, multi-
scale segmentation, reconstruction.
I. I NTRODUCTION
T
O RECOGNIZE the types of aircraft is very important.
We can grasp the activity patterns of aircraft, detect the
unusual trends of aircraft, and make judgment through type
recognition. However, aircraft recognition with high-resolution
spaceborne optical images is a challenging task. It is still
difficult to distinguish targets of some types from the others.
In conventional aircraft recognition methods, several meth-
ods are based on using rotation-invariant features after binariza-
tion. In [1], Hu moment invariant features are extracted from
binary images to automatically identify six aircraft types. In [2],
an independent component algorithm is combined with Zernike
invariant moments for aircraft recognition. In [3], contour track-
ing is used to eliminate much noise first and then uses moment
invariants to recognize the types of the aircraft. These methods
always use thresholding segmentation for the overall silhouette
or shape of targets, and extract rotation-invariant features such
as Hu moments, Zernike moments, wavelet moments, and
Fourier descriptor for recognition. However, these methods
have two drawbacks: 1) obtaining the moment invariants and
Fourier descriptor requires perfect extraction of silhouette or
Manuscript received January 9, 2013; revised May 22, 2013; accepted
June 6, 2013. Date of publication June 24, 2014; date of current version
August 14, 2014. (Corresponding author: H. Sun.)
Q. Wu is with the College of Electronic Science and Engineering, National
University of Defense Technology, Changsha 410073, China.
H. Sun, X. Sun, D. Zhang, K. Fu, and H. Wang are with the Institute of
Electronics, Chinese Academy of Sciences, Beijing 100190, China, and also
with the Key Laboratory of Technology in Geo-spatial Information Processing
and Application System, Chinese Academy of Sciences, Beijing 100190, China
(e-mail: sun.010@163.com).
Color versions of one or more of the figures in this paper are available online
at http://ieeexplore.ieee.org.
Digital Object Identifier 10.1109/LGRS.2014.2328358
shape of each aircraft as a precondition, which is too idealistic
for targets with irregular appearance caused by distortion, low
SNR, and camouflage painting in satellite images; and 2) these
methods do not make full use of the shape characteristics
of aircraft for target representation, which reflects the prior
knowledge of the aircraft target, and will greatly enhance the
robustness of recognition mission.
In addition to the above kind of methods, there are also a
few recognition methods that estimate the direction first after
binarization and then recognize the types of aircraft [4]–[6].
These methods estimate the direction of aircraft before repre-
senting targets that actually takes more aircraft shape charac-
teristics, such as symmetry and fuselage characteristics, into
account. These methods also require the binary image of each
aircraft for direction estimation and the silhouette or contour
with less fracture for target representation, which reduces the
practicability of the above methods.
As aircraft recognition is still a challenging problem, we
want to further investigate how we can resolve issues in this
field. Aircraft recognition is different from other natural object
recognition: 1) the number of aircraft types is limited; and
2) each type of aircraft has fixed size and shape. Considering
the above characteristics, we can build a template for each
type and match the test aircraft to the different types of
templates. By doing this, we can make more use of the shape
characteristics of different types of aircraft. More importantly,
we will focus on how to measure the similarity between targets
and all types of templates, independent of the overall shape
extraction of targets.
In this letter, a novel type recognition approach for aircraft
is proposed. In addition to making more use of the shape
characteristics of different types of aircraft, the advantage of
the approach lies in that it can recognize aircraft robustly
without perfect extraction of silhouette or shape of targets as
a precondition, and can deal with the situation of parts missing
and shadow disturbance. The recognition approach consists of
two steps: direction estimation and type recognition. In the ap-
proach, a direction estimation method is proposed first to align
aircraft to a same direction. Then, a reconstruction-based sim-
ilarity measure is proposed, which transforms the type recog-
nition problem into a reconstruction problem. Finally, a jigsaw
matching pursuit algorithm is proposed to solve the problem.
We evaluate the method using panchromatic 0.6-m-resolution
Quickbird imagery, and the experimental results illuminate that
the method proposed in this letter is effective and accurate.
II. METHODOLOGY
A. Direction Estimation
Considering the shape characteristics of aircraft such as sym-
metry and fuselage characteristics, we estimate the directions
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