id	author	title	date	pages	extension	mime	words	sentence	flesch	summary	cache	txt
american_scientific_journal-5777	Kada, Belkacem 	Design of Flight Control Systems for a Hypersonic Aircraft Using sliding-PID Control	2020	11	.pdf	application/pdf	2828	160	51	On the other hand, hypersonic flows and their impact on the aerodynamics and stability of aerospace vehicles impose more challenges for hypersonic vehicles flight control systems (HV-FCS) designers. Sliding mode control (SMC) strategy has been successfully used to design robust control systems for highly nonlinear systems such as hypersonic vehicles with less performance restrictions and implementation complications.	cache/american_scientific_journal-5777.pdf	txt/american_scientific_journal-5777.txt