Formally Verified Switching Logic for Recoverability of Aircraft Controller
Formally Verified Switching Logic for Recoverability of Aircraft Controller
复制标题
飞机控制器可恢复性的正式验证切换逻辑
DOI:
10.1007/978-3-030-81685-8_27
复制
发表时间:
2021
期刊:
影响因子:
--
通讯作者:
Prabhakar, Pavithra
中科院分区:
文献类型:
--
作者:
Lal, Ratan;McKinnis, Aaron;Hauptman, Dustin;Keshmiri, Shawn;Prabhakar, Pavithra
In this paper, we investigate the design of a safe hybrid controller for an aircraft that switches between a classical linear quadratic regulator (LQR) controller and a more intelligent artificial neural network (ANN) controller. Our objective is to switch safely between the controllers, such that the aircraft is always recoverable within a fixed amount of time while allowing the maximum time of operation for the ANN controller. There is aprioriknown safety zone for the LQR controller operation in which the aircraft never stalls, over accelerates, or exceeds maximum structural loading, and hence, by switching to the LQR controller just before exiting this zone, one can guarantee safety. However, thisprioriknown safety zone is conservative, and therefore, limits the time of operation for the ANN controller. We apply reachability analysis to expand the known safety zone, such that the LQR controller will always be able to drive the aircraft back to the safe zone from the expanded zone (“recoverable zone") within a fixed duration. The “recoverable zone" extends the time of operation of the ANN controller. We perform simulations using the hybrid controller corresponding to the recoverable zone and observe that the design is indeed safe.
DOI:
--
发表时间:
2017
期刊:
International Conference on Tools and Algorithms for Construction and Analysis of Systems
影响因子:
--
作者:
Nima Roohi;P. Prabhakar;Mahesh Viswanathan
通讯作者:
Mahesh Viswanathan