2024 Vol. 50, No. 5

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Volume 5 Issue E-journal
Volume 50 Issue52024
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A review of algorithms for multi-vector attitude synthesis of research
WU Meiping, LIU Yilin, GUO Yan, YU Ruihang
2024, 50(5): 1427-1437. doi: 10.13700/j.bh.1001-5965.2022.0325
Abstract:

The transformation of vector measurements into attitude measurements is known as the Wahba problem in the literature of attitude estimation. This review introduces various algorithms for minimizing the Wahba’s loss function, including estimator of the optimal quaternion (ESOQ), quaternion estimator ...

Image enhancement algorithm for underwater vision based on weighted fusion
BEN Yueyang, TANG Rui, DAI Ping’an, LI Qian
2024, 50(5): 1438-1445. doi: 10.13700/j.bh.1001-5965.2022.0540
Abstract:

Aiming at the problem of poor feature extraction and feature matching in the underwater visual simultaneous localization and mapping (SLAM) front end, an image-enhanced algorithm based on weighted fusion is proposed for the underwater visual SLAM front end. Specifically, the algorithm is based on th...

Vision-based path planning algorithm of unmanned bird-repelling vehicles in airports
WANG Rui, LI Jinming, SHI Yulong, SUN Hui
2024, 50(5): 1446-1453. doi: 10.13700/j.bh.1001-5965.2022.0717
Abstract:

Low-flying birds flying in the vicinity of the airports are a serious threat to the safety of aircraft takeoff and landing, and the existing bird-repelling measurements make it difficult to effectively repel low-flying birds for high instrument resource consumption and large spatio-temporal influenc...

Aircraft system identification algorithm based on generalized equivalent model
ZHOU Dapeng, LI Heqi, WANG Yeguang, WANG Lixin
2024, 50(5): 1454-1462. doi: 10.13700/j.bh.1001-5965.2022.0507
Abstract:

This study provides a frequency domain identification approach aimed at the high-order time-delay model matching problem for complex systems like carrier aircraft. A high-order time-delay model of the complex system is ultimately identified after the generalized frequency-domain identification model...

Consensus control of multi-agent systems with uncertain communication networks
LIU Wei, YAN Shi, WANG Xibin, LI Ruitao, ZHOU Shaolei
2024, 50(5): 1463-1473. doi: 10.13700/j.bh.1001-5965.2022.0518
Abstract:

Under general directed topology conditions, a consensus control approach with uncertainty in communication networks is studied, and a consensus controller based on output feedback is built, with the aim of solving the consensus control problem of a class of Lipschitz nonlinear multi-agent systems. B...

Pinning control of AUV cluster under input delay and communication delay
DU Xue, SUN Zhaodong, XU Chenglong, JIN Zesheng
2024, 50(5): 1474-1480. doi: 10.13700/j.bh.1001-5965.2022.0538
Abstract:

Addressing the impact of latency issues on cluster stability. The traction control strategy is studied. Through the use of feedback linearization, the autonomous underwater vehicle (AUV) model is reduced to a second-order integrator model. The formation control problem of multiple AUV clusters with ...

Obstacle detection and tracking method based on millimeter wave radar and LiDAR
NIU Guochen, TIAN Yibo, XIONG Yu
2024, 50(5): 1481-1490. doi: 10.13700/j.bh.1001-5965.2022.0541
Abstract:

Limited detecting range, low precision, and poor stability are just a few of the issues with obstacle detection and tracking that arise when using a single millimeter wave radar, or LiDAR, on an unmanned vehicle in a park. An obstacle-detecting and tracking approach based on the fusion of radar and ...

A multi-task traffic scene detection model based on cross-attention
NIU Guochen, WANG Xiaonan
2024, 50(5): 1491-1499. doi: 10.13700/j.bh.1001-5965.2022.0610
Abstract:

Perception is the foundation and key issue to autonomous driving, but most single models can’t simultaneously complete multiple detection tasks such as traffic objects, drivable areas, and lane lines. This paper proposes a multi-task traffic scene detection model based on cross-attention, which can ...

Engineering test method for avionics system based on conformity evidence chain
ZHONG Lunlong, ZHANG Zhuoxuan, CHEN Yonggang
2024, 50(5): 1500-1511. doi: 10.13700/j.bh.1001-5965.2022.0643
Abstract:

In order to form logical and traceable airworthiness conformity materials, an engineering test method for an avionics system based on a conformity evidence chain is proposed, and the key problems in the implementation are analyzed and studied. A validation platform based on the specifications of an ...

UAV control law design method based on active-disturbance rejection control
ZUO Ling, ZHANG Xianglun, LI Zhiyu, QIN Wei, HOU Lin, YANG Sen
2024, 50(5): 1512-1522. doi: 10.13700/j.bh.1001-5965.2022.0488
Abstract:

To provided a fast solution to multi-UAV and multi-task flight control law design, this paper presents a control law structure based on the active-disturbance rejection control method, and designs a reusable extended state observer and tracking differentiator. Meanwhile, the application of this meth...

Reconfiguration control and motion simulation of tilt-rotor aircraft with multilinks
WANG Xuqiao, LAI Feilong, ZHAO Changli
2024, 50(5): 1523-1531. doi: 10.13700/j.bh.1001-5965.2022.0522
Abstract:

Multilinks rotorcraft has the characteristic of configuration transformation, which is an effective configuration design method to deal with the variation of motion space. The dynamic reconfiguration flight of Multilinks rotorcraft has a critical configuration interval that cannot be achieved becaus...

Design of a new opening and speed limiting mechanism of passenger door
ZHI Wenjing, LI Jiangang, ZHANG Chen, LIU Dongping, DU Xiujun
2024, 50(5): 1532-1540. doi: 10.13700/j.bh.1001-5965.2022.0714
Abstract:

The passenger door is an important part of the cabin door mechanism of civil aircraft, which directly affects the integrity and safety of the aircraft structure and function. A new opening and limiting device was created to control the falling speed of the passenger door after the causes of the dama...

Formation reconfiguration control of UAV swarm based on MPC-PIO
LIAO Jian, GAO Xiangyang, YAN Shi, ZHOU Shaolei, WANG Donglai, KANG Yuhang
2024, 50(5): 1541-1550. doi: 10.13700/j.bh.1001-5965.2022.0398
Abstract:

To realize security and accurate strikes under the battlefield environment with various obstacles, unmanned aerial vehicle swarm must possess the ability of self-formation reconfiguration. The unmanned aerial vehicle movement model and leader follower swarm formation control structure are establishe...

Rotation binocular stereo rectification algorithm based on hierarchical spatial consistency
LUO Qijun, TIAN Xin, GAO Qingji
2024, 50(5): 1551-1559. doi: 10.13700/j.bh.1001-5965.2022.0611
Abstract:

The mechanical gap of the turntable in the rotating binocular stereo vision system causes the left and right cameras to rotate and deviate in translation, severely distorting the stereo rectification image. To solve this problem, a rotating binocular stereo rectification algorithm based on hierarchi...

Vibration control of flexible spacecraft with output constraints and external disturbances
LIU Shuyang, YANG Honglei, ZHANG Zhenguo, LI Yuanchun
2024, 50(5): 1560-1567. doi: 10.13700/j.bh.1001-5965.2022.0622
Abstract:

A vibration control with direct joint torque input is presented for flexible spacecraft systems subject to external disturbances and output limits. Firstly, the dynamic characteristics of the system are described by a distributed parameter model which is composed of partial differential equation (PD...

Migration control strategy for swarm density based on PDE-constrained heat conduction
PAN Xiao, SONG Ting, LI Meng, YAO Chuang
2024, 50(5): 1568-1575. doi: 10.13700/j.bh.1001-5965.2022.0635
Abstract:

Advances in miniaturization are enabling the development of microscale swam with the advantages of high functional density, lower cost and high flexibility for the potential applications of reconnaissance monitoring, and space offensive and defensive operations. Facing the development trend of space...

Aircraft flight qualities of short take-off and vertical landing
ZHEN Xudong, WANG Zi’an, HU Runchang, GONG Zheng, CHEN Yongliang, WANG Jiangfeng
2024, 50(5): 1576-1585. doi: 10.13700/j.bh.1001-5965.2022.0413
Abstract:

Based on the characteristics of short take-off and vertical landing (STOVL) aircraft, the flight quality requirements of STOVL aircraft are proposed in light of control efficiency and modal characteristics, combined with the AGARD 577 flight quality specification. The control efficiency of the vehic...

Data-driven fault detection and diagnosis for UAV swarms
LI Runze, JIANG Bin, YU Ziquan, LU Ningyun
2024, 50(5): 1586-1592. doi: 10.13700/j.bh.1001-5965.2022.0441
Abstract:

The security requirements of the unmanned aerial vehicle (UAV) swarm system are extremely strict, and real-time fault detection and diagnosis is one of its important supporting technologies. This paper presents a fault diagnosis method based on statistical model and improved broad learning system (B...

UAV three-dimensional path planning based on ε-level bat algorithm
WANG Fuyi, MENG Xiuyun, ZHANG Haikuo
2024, 50(5): 1593-1603. doi: 10.13700/j.bh.1001-5965.2022.0502
Abstract:

To address the problem of complex terrain environment and various threats and constraints, this article proposes a path planning algorithm for UAV based on ε-level improved bat algorithm. First, according to the drone target function and constraints, a three-dimensional path planning model of the UA...

Output regulation adaptive drag-free control with enhanced Kinky Inference
SUN Xiaoyun, SHEN Qiang, WU Shufan
2024, 50(5): 1604-1613. doi: 10.13700/j.bh.1001-5965.2022.0504
Abstract:

Achieving ultra-precision and ultra-stable requirements is challenging in the space gravitational wave detection mission due to complex disturbances present in the spacecraft's internal test masses, including load hardware noise, environmental noise, and micro-thrust coupling noise.These disturbance...

An online compensation method for random error of optical gyro
LU Kewen, WANG Xinlong, WANG Bin, DING Xiaokun, HU Xiaodong
2024, 50(5): 1614-1619. doi: 10.13700/j.bh.1001-5965.2022.0523
Abstract:

The random error online compensation method of optical gyro establishes a random error model offline and compensates random error online by Kalman filter. However, when used for online compensation, the offline random error model has deviation due to the influence of the external environment and the...

RBF neural network robust adaptive control of quadrotor aircraft
MA Zhenwei, BAI Hao, CHEN Hongbo, WANG Jinbo
2024, 50(5): 1620-1628. doi: 10.13700/j.bh.1001-5965.2022.0595
Abstract:

The paper presents a robust adaptive global control method based on radial basis function (RBF) neural network for quadrotors with model uncertainties and bounded external disturbances. The method combines the strong fitting ability of neural network control to unknown nonlinearities and the global ...

Robust anti-swing technology for helicopter slung load based on wave control
LI Honghong, HAN Yanhua
2024, 50(5): 1629-1638. doi: 10.13700/j.bh.1001-5965.2022.0326
Abstract:

Application of helicopter to transport heavy and bulky loads creates various stability problems especially during maneuvering from level flight to hovering; thus, it is significant to reduce the swing amplitude of suspended loads. An anti-swing controller is designed for a helicopter with slung load...

Air gap flux-oriented vector control techniques of wind power synchronous motor
WANG Jiahao, TIAN Yuru, YU Naizhao
2024, 50(5): 1639-1645. doi: 10.13700/j.bh.1001-5965.2022.0463
Abstract:

Wind energy is one of the most promising renewable energy sources in China, and the main factors affecting the application of wind energy conversion are the control method and characteristics of wind turbines. This study proposes a vector control technique based on air gap flux orientation, addressi...

Formation control and aggregation method of UAV based on consensus theory
GOU Jinzhan, LIANG Tianjiao, TAO Chenggang, MA Bo, WANG Haifeng, WU Yu
2024, 50(5): 1646-1654. doi: 10.13700/j.bh.1001-5965.2022.0470
Abstract:

According to the characteristics of unmanned aerial vehicle kinematics model and the problem of remote forming, an improved consensus-based algorithm was proposed to solve the gathering-forming strategy of unmanned aerial vehicle. The coordinate system which can describe the formation directly was e...

Effectiveness evaluation method for earth observation satellite attitude control system
CAO Yin, CHENG Yuehua, GAO Bo, ZHANG Yanhua, XU Guili
2024, 50(5): 1655-1664. doi: 10.13700/j.bh.1001-5965.2022.0489
Abstract:

The problem of satellite system effectiveness assessment is the basis of satellite efficiency improvement and satellite program optimization design. Taking the attitude control system for earth observation satellite attitude control system as the object of effectiveness assessment, an analysis of sa...

Quadrotor sliding mode control based on predefined time
LIU Hao, HUANG Shan, TU Haiyan
2024, 50(5): 1665-1674. doi: 10.13700/j.bh.1001-5965.2022.0481
Abstract:

To address the control problem of the position loop and attitude loop of the quadrotor, so that the position and attitude of the quadrotor can be stable in the predetermined time, a position and attitude controller based on the predefined time sliding mode control algorithm is proposed. By controlli...

Motion analysis and gait planning of a novel revolving wheel-legged robot
ZHANG Chengyao, WANG Gang, CHE Honglei, LI Wenjun
2024, 50(5): 1675-1684. doi: 10.13700/j.bh.1001-5965.2022.0491
Abstract:

To address the problems of the existing quadruped robot's insufficient obstacle surmounting ability and unstable obstacle surmounting, a new wheel-legged robot was proposed to achieve high obstacle surmounting and stable centroid through wheel-train transmission. Adopting the wheel configuration, th...

Distributed adaptive anti-disturbance control for power systems based on multi-agents
SHI Tongxin, CHEN Longsheng, LI Tongshuai, JIN Feiyu
2024, 50(5): 1685-1692. doi: 10.13700/j.bh.1001-5965.2022.0496
Abstract:

In response to problems like the inevitable nonlinearities, uncertainties and dynamic external disturbances in multi-machine power systems, a distributed adaptive anti-disturbance control scheme is proposed based on radial basis function neural networks (RBFNN) and nonlinear disturbance observers (N...

Intelligent solution method based on high-speed aircraft fire control model
YANG Ben, JIN Feiteng, LIU Yanbin, CHEN Boyi, PENG Shouyong
2024, 50(5): 1693-1701. doi: 10.13700/j.bh.1001-5965.2022.0503
Abstract:

This paper studies the fire control calculation problem of air-breathing high-speed aircraft. High-speed aircraft has higher requirements for the fire control model calculation, a more complicated flying environment, and a shorter response time than traditional subsonic and supersonic combat aircraf...

Fixed-time formation control of quadrotor UAV swarm with unknown disturbances
ZHENG Weiming, XU Yang, LUO Delin
2024, 50(5): 1702-1712. doi: 10.13700/j.bh.1001-5965.2022.0506
Abstract:

A fixed-time formation control approach is proposed for the formation control of underactuated nonlinear quadrotor UAV swarm with unknown disturbances. Firstly, a distributed fixed-time sliding mode estimator is designed. Each UAV can quickly estimate its own desired position information under the c...

Model-free adaptive cascade control for temperature system of a hot wind tunnel
CHEN Jiacheng, YANG Xu, MA Yuxiang, LI Dong, DONG Sujun, LI Yunhua
2024, 50(5): 1713-1720. doi: 10.13700/j.bh.1001-5965.2022.0528
Abstract:

For the dynamic calibration of high-temperature thermocouples, the thermal strength test of aero-engine blades, and other application scenarios, the thermal wind tunnel can offer a well-distributed and stable temperature field. How to control the thermal flow generated by thermal wind tunnel in a wi...

Improved predictor-corrector guidance method for time-coordination entry
GAO Yuan, HU Yu, CHEN Jinyong, ZHANG Jie, ZHOU Rui
2024, 50(5): 1721-1730. doi: 10.13700/j.bh.1001-5965.2022.0530
Abstract:

For the hypersonic vehicle, a time coordination predictor-corrector guidance approach based on an open-loop coordination structure is presented to achieve the time coordination of the entry gliding process. The guidance method does not depend on real-time communication between the vehicles. The long...

A comprehensive air-ground target attackability value ranking based on comprehensive weighting
SUN Xue’an, WANG Yin, ZHOU Qixian
2024, 50(5): 1731-1737. doi: 10.13700/j.bh.1001-5965.2022.0539
Abstract:

In the area of intelligent warfare, unmanned system combat capabilities have increasingly become an important factor in the military strength of major powers. When utilizing unmanned aerial vehicles for air-to-ground assault operations, it is imperative to assess and prioritize the enemy’s ground ta...

Flight data anomaly detection based on correlation parameter selection
ZHONG Jie, LUO Chong, ZHANG Heng, MIAO Qiang
2024, 50(5): 1738-1745. doi: 10.13700/j.bh.1001-5965.2022.0574
Abstract:

With the maturity of unmanned aerial vehicle (UAV) technology, UAVs are being used more and more widely in the military and civilian fields. Meanwhile, the safety of UAV is gradually being emphasized. The health of the UAV’s flight can be immediately reflected in its flight data. Anomaly detection r...

Altitude control strategy for high-aspect-ratio wings with active morphing
SHE Wanqiang, LIU Yanbin, CHEN Boyi
2024, 50(5): 1746-1752. doi: 10.13700/j.bh.1001-5965.2022.0612
Abstract:

This paper proposed a deformation-aided altitude control strategy for the high aspect ratio aircraft to address the flight control problem of the structure/flight coupling dynamics. Based on the assumption of element wings, the dihedral deformation of high aspect ratio aircraft are constructed, and ...

Fault diagnosis of gearbox under open set and cross working condition based on transfer learning
MA Xiang, XU Shu, SHANG Pengchao, MA Jian, ZHOU Ruzhi
2024, 50(5): 1753-1760. doi: 10.13700/j.bh.1001-5965.2022.0719
Abstract:

With the continuous development of industry and aerospace technology, the working conditions and failure modes of rotating machinery are becoming increasingly diversified and complex, and reliability and safety problems are becoming increasingly prominent. It is critical to research efficient fault ...