Suboptimal Impact-Angle-Constrained Guidance Law Using Linear Pseudospectral Model Predictive Spread Control
This paper aims at proposing a nonlinear suboptimal impact-angle-constrained guidance law for an interceptor engaging against an incoming high-speed ballistic missile in three dimensions. The method is based on an improved Linear Pseudospectral Model Predictive Control (LPMPC), in which the control...
Main Authors: | Xingcai He, Wanchun Chen, Liang Yang |
---|---|
Format: | Article |
Language: | English |
Published: |
IEEE
2020-01-01
|
Series: | IEEE Access |
Subjects: | |
Online Access: | https://ieeexplore.ieee.org/document/9104730/ |
Similar Items
-
Entry Guidance With No-Fly Zone Avoidance Using Linear Pseudospectral Model Predictive Control
by: Liang Yang, et al.
Published: (2019-01-01) -
Near Optimal Explicit Guidance Law with Impact Angle Constraints for a Hypersonic Re-entry Vehicle
by: Kalirajan KARTHIKEYAN, et al.
Published: (2018-06-01) -
Time-Optimal Guidance for Impact Angle Constrained Interception of Moving Targets
by: Akhil, G
Published: (2018) -
Numerical Investigation of Inclination on the Thermal Performance of Porous Fin Heatsink using Pseudospectral Collocation Method
by: George Oguntala, et al.
Published: (2019-03-01) -
Guidance Laws For Impact Angle Constraints And Exo-Atmospheric Engagements
by: Ratnoo, Ashwini
Published: (2010)