2021 Vol. 47, No. 2

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Volume 47 Issue22021
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Ground- and ship-based guidance approaches for autonomous landing of UAV
SHEN Lincheng, KONG Weiwei, NIU Yifeng
2021, 47(2): 187-196. doi: 10.13700/j.bh.1001-5965.2020.0280
Abstract:

In recent years, with the rapid development of autonomous control technology and mission loads, more and more Unmanned Aerial Vehicles (UAVs) have mission autonomy capability. During the execution of the mission, the safety risk of the landing phase is the greatest, and poor navigation and positioni...

A reentry steady glide guidance algorithm based on fuzzy control
ZHOU Rui, ZHANG Yuhang, XIONG Wei, SHI Zhiguang
2021, 47(2): 197-206. doi: 10.13700/j.bh.1001-5965.2020.0264
Abstract:

Considering the periodic oscillation in reentry glide of Lifting Hypersonic Vehicle (LHV), a feedback correction method based on fuzzy logic and fuzzy control is proposed to reduce the oscillation and keep reentry glide trajectory smooth. First, the longitudinal guidance is developed based on the pr...

Three-dimensional vibration measurement method for lightweight beam based on machine vision
PENG Cong, MIAO Weidong, ZENG Cong
2021, 47(2): 207-212. doi: 10.13700/j.bh.1001-5965.2020.0211
Abstract:

Vibration measurement is one of the methods of state detection and fault diagnosis. In view of the loading effect in the current contact vibration measurement method and other problems, this paper studies the three-dimensional vibration measurement method based on machine vision. First, based on the...

Design of underwater-launched controller for small rotor UAV
WU Jiang, CHEN Enmin, GAO Yijie, LIU Yipeng, GAO Xin, XIA Jie
2021, 47(2): 213-222. doi: 10.13700/j.bh.1001-5965.2020.0281
Abstract:

The attitude stability of the underwater-launched small rotor UAV directly affects the result of the entire submarine launch task. Aimed at the problems that the rotor UAV's attitude is difficult to adjust quickly during the launching period, and the initial launch attitude is easily interfered by o...

Path planning method for spacecraft formation reconfiguration based on CGAPIO
HUA Bing, SUN Shenggang, WU Yunhua, CHEN Zhiming
2021, 47(2): 223-230. doi: 10.13700/j.bh.1001-5965.2020.0277
Abstract:

Aimed at the path planning problem of spacecraft formation reconfiguration, an Adaptive Pigeon-Inspired Optimization algorithm based on Chaos initialization and Gaussian disturbance (CGAPIO)is proposed.In order to make the initial value of the pigeons more diverse and uniform, the Tent Map chaotic m...

Maneuver trajectory optimization method of multicopter under space-time constraints
CAI Zhihao, ZUO Yiming, WANG Yingxun
2021, 47(2): 231-239. doi: 10.13700/j.bh.1001-5965.2020.0272
Abstract:

Multicopter are often used in complex and variable scenarios such as post-earthquake search and rescue, geological exploration, etc. Considering their endurance and environmental characteristics, optimizing the flight trajectory of multicopter to complete tasks better and faster has become a key iss...

Performance reliability of multi-state navigation system based on T-S fuzzy fault tree
LIU Yong, LUO Delin, SHI Cui, WU Huaxin
2021, 47(2): 240-246. doi: 10.13700/j.bh.1001-5965.2020.0276
Abstract:

The T-S fuzzy fault tree model is applied to the performance analysis of the multi-state navigation system, considering that complex multi-state system has different performance reliability in different fault states. The T-S fuzzy fault tree is used to represent the performance variables of the syst...

High-g maneuver dynamic surface control of fighter plane under input saturation
ZHOU Zhangyong, SHAO Shuyi, HU Wei
2021, 47(2): 247-254. doi: 10.13700/j.bh.1001-5965.2020.0209
Abstract:

An adaptive neural network dynamic surface control method is proposed to resolve the input saturation problem of aircraft high- g maneuver flight. The Radial Basis Function (RBF) neural networks are utilized to approximate the unknown uncertain parts of aircraft model. The hyperbolic tangent functio...

Guidance law design based on stochastic maneuvering model and impact point predictions
YANG Shu
2021, 47(2): 255-261. doi: 10.13700/j.bh.1001-5965.2020.0202
Abstract:

A novel guidance law design method based on impact point predictions is proposed in this paper. A stochastic maneuvering model and the adaptive Kalman filter are used to estimate the projectile states, and predicted impact points are solved analytically. Guidance commands are generated based on erro...

Control strategy and simulation for probe-and-drogue aerial autonomous refueling
HUA Yixin, ZOU Quan, TIAN Haiming
2021, 47(2): 262-270. doi: 10.13700/j.bh.1001-5965.2020.0213
Abstract:

The probe-and-drogue Aerial Autonomous Refueling (AAR) technology has been widely studied because it requires little modification of refueling equipment and can be applied to a variety of refueling processes. However, there are few researches on the whole flight control process from take-off to dise...

Time-varying formation H control for air unmanned swarm system
KANG Yuhang, DAI Hongde, QI Yahui, ZHANG Bangchu, LIU Xuanbing, CHENG Jun
2021, 47(2): 271-280. doi: 10.13700/j.bh.1001-5965.2020.0200
Abstract:

This paper studies the time-varying formation H control problem for Air Unmanned Swarm System (AUSS) under directed communication topology, corrupted by communication delay and external disturbances. First, based on the expected formation configuration information of swarm system, the real-time sta...

ADRC-based roll-yaw coupling control of underactuated moving mass flight vehicles
LIU Zhitao, LI Jianqing, GAO Changsheng
2021, 47(2): 281-288. doi: 10.13700/j.bh.1001-5965.2020.0206
Abstract:

Considering the underactuated problem of flight vehicles with single moving mass roll control system, this paper proposes a controller based on the idea of active disturbance rejection, which achieves the command roll angle tracking and sideslip angle stabilization control only with the laterally co...

Trajectory control method for unmanned carrier aircraft taxiing
LIANG Tianjiao, CHEN Xiaoming, YANG Zhaoxu, WANG Haifeng, LIANG Qing
2021, 47(2): 289-296. doi: 10.13700/j.bh.1001-5965.2020.0294
Abstract:

Unmanned aircraft is an important weapon of carrier-aircraft system. Autonomous taxiing of aircraft is significant for the efficiency of deck operation. The trajectory control problem of unmanned aircraft taxiing on deck of an aircraft carrier is studied in this paper. First, the task of aircraft ta...

Weapon-target assignment in UAV cluster based on pheromone heuristic wolf pack algorithm
LIU Senqi, WANG Hong, YU Ningyu, HAO Likai
2021, 47(2): 297-305. doi: 10.13700/j.bh.1001-5965.2020.0208
Abstract:

Unmanned Aerial Vehicle (UAV) cluster operation is an important mode of intelligent warfare in the future. In order to give full play of the overall operational advantages of UAV cluster, a mathematical model is constructed to solve the Weapon-Target Assignment (WTA) problem in UAV cluster attacks a...

Unmanned vehicle positioning and mapping method based on multi-constraint factor graph optimization
NIU Guochen, WANG Yu
2021, 47(2): 306-314. doi: 10.13700/j.bh.1001-5965.2020.0212
Abstract:

Aimed at the problem that the current low-speed positioning system of unmanned vehicle extremely relies on the Global Navigation Satellite System (GNSS), which has low positioning accuracy, large drift error and serious environmental impact, a low-cost and high-precision positioning and mapping meth...

Distributed optimal rendezvous of multi-UAV systems in prescribed time based on time-domain mapping
DING Chao, WEI Ruixuan, ZHOU Kai
2021, 47(2): 315-322. doi: 10.13700/j.bh.1001-5965.2020.0215
Abstract:

To solve the prescribed-time optimal rendezvous problem for multi-UAV systems, a distributed optimization framework is established based on time-domain transformation technique. By introducing a specific time-domain transformation, the prescribed-time decision problem in original time-domain is tran...

Distributed event-triggered group attitude coordinated control of multi-spacecraft
WANG Shuailei, ZHOU Shaolei, DAI Feiyang, LIU Wei, YAN Shi
2021, 47(2): 323-332. doi: 10.13700/j.bh.1001-5965.2020.0266
Abstract:

Group attitude coordinated control of multi-spacecraft on the basis of distributed event-triggered mechanism is investigated. The multi-spacecraft system contains several subgroups, and the information exchange among spacecraft is regarded as undirected topology. The attitude of spacecraft is descri...

Satellite time series data classification method based on trend symbolic aggregation approximation
RUAN Hui, LIU Lei, HU Xiaoguang
2021, 47(2): 333-341. doi: 10.13700/j.bh.1001-5965.2020.0332
Abstract:

As the main symbolic representation method widely used in time series data mining, the Symbolic Aggregation Approximation (SAX) uses the mean value of segments as the symbolic representation. Since it is impossible to distinguish different time series that have different trends but the same mean val...

Visualization and noise reduction algorithm based on event camera
YAN Changda, WANG Xia, ZUO Yifan, LI Leilei, CHEN Jiabin
2021, 47(2): 342-350. doi: 10.13700/j.bh.1001-5965.2020.0192
Abstract:

To overcome the problem that the asynchronous event stream generated by the event camera is hard to observe, utilize and there is a lot of noise, we introduce an improved visualization and noise reduction algorithm for the event camera. Because the event stream reacts to the object movement, the pro...

A smooth Sun-pointing guidance method for satellites constrained by deviation of Earth-pointing
JI Haoran, HUANG Di
2021, 47(2): 351-358. doi: 10.13700/j.bh.1001-5965.2020.0293
Abstract:

Under traditional Sun-pointing guidance method constrained by the deviation of Earth-pointing, the expected attitude of the satellite would rapidly flip when the angle between the satellite-Sun line and the satellite-Earth line reaches the extreme value, leading to the large peak power consumption a...

Real-time obstacle avoidance algorithm based on pigeon-inspired optimization
LI Shuanglin, HE Jiahao, AO Haiyue, LIU Yanbin
2021, 47(2): 359-365. doi: 10.13700/j.bh.1001-5965.2020.0198
Abstract:

In order to ensure that the mobile robot can reach the target position without collisions, this paper proposes a real-time obstacle avoidance algorithm that integrates the pigeon-inspired optimization into the Circle Sector Expansion plus (CSE+) method. This algorithm includes a judgment mechanism t...

Survivability of underwater communication system based on node connectivity
WANG Yida, LIANG Qingwei, ZHANG Xin
2021, 47(2): 366-372. doi: 10.13700/j.bh.1001-5965.2020.0210
Abstract:

In the underwater communication system, it is one-sided to describe the importance of each node in the underwater communication system only by considering the strength of the node. In order to better evaluate the importance of the node in the underwater communication system, this paper proposes the ...

Maneuvering flight control of QUAV based on bi-directional motor actuation
XU Lihao, ZHANG Yu, XU Bin
2021, 47(2): 373-381. doi: 10.13700/j.bh.1001-5965.2020.0221
Abstract:

The position and attitude control of Quadrotor Unmanned Aerial Vehicle (QUAV) determines its maneuverability. First, to overcome the mobility defect of the under-actuated system, the dynamic model of bi-directional-motor-driven QUAV based on quaternion is presented, including the analysis on omnidir...

Event-triggered attitude control of liquid-filled spacecraft
DONG Xinlei, QI Ruiyun, LU Shan, WANG Huanjie
2021, 47(2): 382-390. doi: 10.13700/j.bh.1001-5965.2020.0282
Abstract:

Aimed at the attitude system of liquid-filled spacecraft with large-amplitude liquid sloshing and limited communication resources, a control strategy combining adaptive sliding mode control and event-triggering mechanism is proposed. First, sliding mode variable structure control is used to weaken t...

Unmanned aerial vehicle swarm formation control based on paired interaction mechanism in jackdaws
ZHANG Ling, DUAN Haibin, YONG Ting, DENG Yimin, WEI Chen
2021, 47(2): 391-397. doi: 10.13700/j.bh.1001-5965.2020.0265
Abstract:

Inspired by the paired flight mechanism of jackdaws, a paired interactive swarm model is proposed and applied to the Unmanned Aerial Vehicle (UAV) swarm control system. Firstly, by imitating the paired interaction between jackdaw individuals, the neighbor selection mechanism is designed in pairing i...

An analytical predictor-corrector guidance method designed for spacecraft reentry with short range
ZHOU Liang, ZHANG Hongbo
2021, 47(2): 398-405. doi: 10.13700/j.bh.1001-5965.2020.0318
Abstract:

For the manned lunar return spacecraft reentry problem, an analytical predictor-corrector guidance method for short range reentry is proposed. Firstly, the concept of glide reentryis introduced, which has been studied in the trajectory design of high lift-to-drag ratio vehicle.In order to pre-design...

Trajectory planning of unmanned helicopter formation based on improved artificial fish swarm algorithm
MA Ziyuan, GONG Huajun, WANG Xinhua
2021, 47(2): 406-413. doi: 10.13700/j.bh.1001-5965.2020.0203
Abstract:

To solve formation path planning problem of the Unmanned Helicopter (UH), a path planning algorithm is proposed based on improved Artificial Fish Swarm Algorithm (AFSA). An adaptive vision model of artificial fish for artificial fish swarm algorithm was put forward from two aspects of neighborhood l...

Trajectory tracking control and optimal computation of attraction domain for aircraft in perching maneuvers
WANG Wutian, HE Zhen, YUE Cheng
2021, 47(2): 414-423. doi: 10.13700/j.bh.1001-5965.2020.0207
Abstract:

For the longitudinal movement of fixed-wing aircraft in perching maneuvers, the perching trajectory control design and the optimization method of attraction domains are investigated. First, according to the perching dynamics model and the constraints of states during the perching, the nominal trajec...

Swarm rounding up method of UAV based on situation cognition
WU Zichen, HU Bin
2021, 47(2): 424-430. doi: 10.13700/j.bh.1001-5965.2020.0274
Abstract:

UAV swarm rounding up is an important mission mode of intelligent UAV swarm operation. Most of the existing swarm rounding up methods are based on the known environment, and the strategy often fails in the face of unknown mission environment. To solve this problem, a developmental model based on sit...