Single Network Adaptive Critic (SNAC) Design for a Morphing Aircraft

Nobleheart, Wilfred; Geethalakshmi, L; Chakravarthy, Animesh; Steck, James E.

doi:10.2514/6.2012-4614

Cited by 1 publication

(1 citation statement)

References 14 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

“…A joint simulation method based on Missile DATCOM and MATLAB proposed by Zhang Fair is applied to the study of variable wing dynamic characteristics of typical axisymmetric missiles [16]. Nobleheart et al designed a time-varying system for a single-neural network adaptive controller for morphing aircraft [17]. In terms of the control of the morphing aircraft, Dong et al studied the smooth-switching linear variable parameter (LPV) H∞ control problem for a class of variable span aircraft to ensure the stability and robustness of the aircraft system [18].…”

Section: Introductionmentioning

confidence: 99%

Integrated Guidance and Control for Hypersonic Morphing Missile Based on Variable Span Auxiliary Control

Bao

Wang

Tang

2019

International Journal of Aerospace Engineering

View full text Add to dashboard Cite

The morphing aircraft can improve the flight performance of hypersonic vehicles by satisfying the flight requirements of large airspace and large velocity field. In this paper, for the hypersonic variable span missile, the dynamic model and aerodynamic model are established on the variable span characteristic. The adaptive dynamic surface control back-stepping method is used to establish the integrated guidance and control (IGC) with terminal angular constraint in the dive phase of the hypersonic variable span missile. The span variety is used to assist the lift control to achieve fast and stable control for the centroid motion. The simulation results demonstrate that the feasibility and robustness of the IGC method of the hypersonic variable span missile is better than the invariable span.

show abstract

Section: Introductionmentioning

confidence: 99%