TY - JOUR
T1 - Unified Method for Field-of-View-Limited Homing Guidance
AU - Dong, Wei
AU - Wang, Chunyan
AU - Wang, Jianan
AU - Son, Hungsun
AU - Xin, Ming
N1 - Publisher Copyright:
© 2022 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
PY - 2022
Y1 - 2022
N2 - Homing guidance requires maintaining the target lock-on condition within the seeker’s field of view (FOV). This paper aims at developing a unified FOV-limited guidance framework from which a variety of two-dimensional (2D) and three-dimensional (3D) guidance laws can be derived. First, the unified method for 2D homing guidance is established by augmenting an arbitrary baseline guidance law with a biased command. To mitigate the effect on the baseline guidance law, this biased command is designed in the admissible range that respects the FOV limit and only takes effect when the lead angle approaches the FOV bound. For more practical relevance, the autopilot dynamic of any order is further considered explicitly in the design with a recursive approach. Then, the unified method for 3D homing guidance with coupling nonlinearity is developed by exploiting the geometric relation among space angles. Unlike existing similar results, the proposed design requires neither switch logic nor numerical algorithms, which allows for continuous guidance command and convenient implementation. With the proposed method, various illustrative guidance laws are derived to demonstrate the significance of the unified framework. Finally, numerical simulations with comparative study are conducted to support the analytical findings and show the superiority of the proposed method.
AB - Homing guidance requires maintaining the target lock-on condition within the seeker’s field of view (FOV). This paper aims at developing a unified FOV-limited guidance framework from which a variety of two-dimensional (2D) and three-dimensional (3D) guidance laws can be derived. First, the unified method for 2D homing guidance is established by augmenting an arbitrary baseline guidance law with a biased command. To mitigate the effect on the baseline guidance law, this biased command is designed in the admissible range that respects the FOV limit and only takes effect when the lead angle approaches the FOV bound. For more practical relevance, the autopilot dynamic of any order is further considered explicitly in the design with a recursive approach. Then, the unified method for 3D homing guidance with coupling nonlinearity is developed by exploiting the geometric relation among space angles. Unlike existing similar results, the proposed design requires neither switch logic nor numerical algorithms, which allows for continuous guidance command and convenient implementation. With the proposed method, various illustrative guidance laws are derived to demonstrate the significance of the unified framework. Finally, numerical simulations with comparative study are conducted to support the analytical findings and show the superiority of the proposed method.
UR - http://www.scopus.com/inward/record.url?scp=85134187487&partnerID=8YFLogxK
U2 - 10.2514/1.G006710
DO - 10.2514/1.G006710
M3 - Article
AN - SCOPUS:85134187487
SN - 0731-5090
VL - 45
SP - 1415
EP - 1434
JO - Journal of Guidance, Control, and Dynamics
JF - Journal of Guidance, Control, and Dynamics
IS - 8
ER -