Discrete-Time Angle Constraint Interception with Model-Assisted Target Maneuver Estimator
This paper investigates the problem of designing angle constraint guidance law against unknown maneuvering targets based on discrete-time sliding mode control theory. Invoking the fact that the future course of action of the target, an independent entity, cannot be predicted beforehand due to its co...
Main Authors: | Y. I. Sheng, W. A. N. G. Jiang, Pei Pei, Zhou Yongjia |
---|---|
Format: | Article |
Language: | English |
Published: |
Hindawi Limited
2020-01-01
|
Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2020/1764510 |
Similar Items
-
Cooperative Intercepting Guidance Law for Large Maneuvering Target with Impact Angle Constraint
Published: (2020-12-01) -
Design of Missile Guidance Laws to Intercept Maneuvering Target
by: Chien-Sheng Lu, et al.
Published: (2004) -
Novel Controller Design for Missiles to Intercept Maneuvering Target
by: Ming-Hsiung Hsueh, et al.
Published: (2007) -
Suboptimal Midcourse Guidance with Terminal-Angle Constraint for Hypersonic Target Interception
by: Shizheng Wan, et al.
Published: (2019-01-01) -
Fixed-Time Cooperative Guidance Law With Angle Constraint for Multiple Missiles Against Maneuvering Target
by: Liang Jing, et al.
Published: (2020-01-01)