DocumentCode
3564604
Title
Hybrid reentry guidance based on reference-trajectory and predictor-corrector
Author
Liang Zixuan ; Ren Zhang ; Bai Chen ; Xiong Zihao
Author_Institution
Sci. & Technol. on Aircraft Control Lab., Beihang Univ., Beijing, China
fYear
2013
Firstpage
4870
Lastpage
4874
Abstract
According to the shortcoming of the conventional guidance, a hybrid reentry guidance algorithm based on the reference-trajectory and the predictor-corrector is presented for the reentry vehicles. The guidance system is separately designed in the longitudinal plane and the lateral plane. Two kinds of the longitudinal guidance laws are studied: one guidance law via the linear quadratic regulator (LQR) and another via the fuzzy logic. A switch law between the two different guidance laws is designed based on the trajectory feature points. To test the capacity of the hybrid guidance method, the Monte Carlo simulations are taken. The proposed hybrid guidance method and the two conventional methods are simulated and compared. The result indicates that the hybrid reentry guidance law has less computing time, high guidance precision, and good robustness.
Keywords
Monte Carlo methods; aircraft control; fuzzy logic; linear quadratic control; predictor-corrector methods; LQR; Monte Carlo simulation; fuzzy logic; guidance system design; hybrid reentry guidance algorithm; lateral plane; linear quadratic regulator; longitudinal guidance laws; longitudinal plane; predictor corrector; reentry vehicles; reference trajectory; switch law; Aerospace control; Digital TV; Electronic mail; Fuzzy logic; Laboratories; Regulators; Vehicles; Fuzzy logic; LQR; Predictor-corrector; Reentry guidance; Reference-trajectory;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2013 32nd Chinese
Type
conf
Filename
6640283
Link To Document