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WEN, Qiuqiu
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1

Learning-based design optimization of second-order tracking..:

Wen, Qiuqiu ; Wang, Mingkai ; Li, Xin.
Aerospace Science and Technology.  137 (2023)  - p. 108302 , 2023
Link: https://doi.org/10.1016/..
 
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2

Impact time control using biased proportional navigation fo..:

SUN, Guoxin ; WEN, Qiuqiu ; XU, Zhiqiang.
Chinese Journal of Aeronautics.  33 (2020)  3 - p. 956-964 , 2020
Link: https://doi.org/10.1016/..
 
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3

Multiple-constraint cooperative guidance based on two-stage..:

DONG, Wei ; WEN, Qiuqiu ; XIA, Qunli.
Chinese Journal of Aeronautics.  33 (2020)  1 - p. 296-307 , 2020
Link: https://doi.org/10.1016/..
 
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4

Stability analysis of spinning missiles induced by seeker d..:

Li, Wei ; Wen, Qiuqiu ; Yang, Yu
Aerospace Science and Technology.  90 (2019)  - p. 194-208 , 2019
Link: https://doi.org/10.1016/..
 
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5

The Impact angle guidance law Parameter design strategy Con..:

, In: 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC),
Lee, BoYa ; Wen, Qiuqiu ; Zhou, Guanqun - p. 1-6 , 2018
Link: https://doi.org/10.1109/..
 
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6

Nonlinear dynamics of a flapping rotary wing: Modeling and ..:

WEN, Qiuqiu ; GUO, Shijun ; LI, Hao.
Chinese Journal of Aeronautics.  31 (2018)  5 - p. 1041-1052 , 2018
Link: https://doi.org/10.1016/..
 
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7

Adaptive weighting impact angle optimal guidance law consid..:

School of Aerospace Engineering, Beijing Institute of technology, Beijing 100081, China ; LI, Ran ; WEN, Qiuqiu...
Journal of Systems Engineering and Electronics.  29 (2018)  1 - p. 142-151 , 2018
Link: https://doi.org/10.21629..
 
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8

Beam-pointing error compensation method of phased array rad..:

WEN, Qiuqiu ; LU, Tianyu ; XIA, Qunli.
Chinese Journal of Aeronautics.  30 (2017)  3 - p. 1217-1230 , 2017
Link: https://doi.org/10.1016/..
 
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9

The effect of phantom-bit technology on the performance of ..:

Lu, Tianyu ; Wen, Qiuqiu ; Yin, Jian
Optik.  127 (2016)  20 - p. 9996-10003 , 2016
Link: https://doi.org/10.1016/..
 
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10

An Approximate Optimal Maximum Range Guidance Scheme for Su..:

Zhang, Dao-Chi ; Xia, Qun-Li ; Wen, Qiu-Qiu.
International Journal of Aerospace Engineering.  2015 (2015)  - p. 1-8 , 2015
Link: https://doi.org/10.1155/..
 
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11

Extended optimal guidance law with impact angle and acceler..:

Li, Ran ; Xia, Qunli ; Wen, Qiuqiu
Journal of Systems Engineering and Electronics.  25 (2014)  5 - p. 868-876 , 2014
Link: https://doi.org/10.1109/..
 
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12

Three-dimensional impact angle constrained distributed coop..:

Wei, Li ; Qiuqiu, Wen ; Lei, He.
Journal of Systems Engineering and Electronics.  32 (2021)  2 - p. 447-459 , 2021
Link: https://doi.org/10.23919..
 
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13

Relative motion and thrust estimation of a non-cooperative ..:

Guang, Zhai ; Hanyu, Zhao ; Qiuqiu, Wen.
Acta Astronautica.  162 (2019)  - p. 98-108 , 2019
Link: https://doi.org/10.1016/..
 
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14

Nonlinear dynamics of a flapping rotary wing: Modeling and ..:

Wen, Qiuqiu ; Guo, Shijun ; Li, Hao.
Qiuqiu Wen, Shijun Guo, Hao Li and Wei Dong. Nonlinear dynamics of a flapping rotary wing: Modeling and optimal wing kinematic analysis. Chinese Journal of Aeronautics, Volume 31, Issue 5, May 2018, Pages 1041-1052.  , 2018
Link: https://doi.org/10.1016/..
 
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15

An Approximate Optimal Maximum Range Guidance Scheme for Su..:

Dao-Chi Zhang ; Qun-Li Xia ; Qiu-Qiu Wen.
http://dx.doi.org/10.1155/2015/389751.  , 2015
Link: https://doi.org/10.1155/..
 
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