51. Receding horizon guidance laws for constrained missiles with autopilot lags
- Author
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Tae-Woong Yoon, Ki Baek Kim, and Wook Hyun Kwon
- Subjects
Scheme (programming language) ,Mathematical optimization ,Horizon (archaeology) ,Computer science ,Applied Mathematics ,Linear matrix inequality ,State (functional analysis) ,Computer Science Applications ,Weighting ,law.invention ,Matrix (mathematics) ,Control and Systems Engineering ,Control theory ,law ,Autopilot ,Minification ,Electrical and Electronic Engineering ,computer ,computer.programming_language - Abstract
In this paper, a new stabilizing receding horizon control (RHC) scheme is proposed for linear continuous time-invariant systems with input and state constraints. The control scheme is based on the minimization of the finite horizon cost with a finite terminal weighting matrix subject to constraints. A new algorithm is suggested to implement the RHC scheme for a constrained receding horizon guidance law (CRHG). The proposed CRHG, which does not use information on the time-to-go, is obtained by using linear matrix inequality (LMI) optimization. Through simulation examples, the performance of the proposed CRHG is illustrated.
- Published
- 2001
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