Title :
Feedback Control for Fuel-Optimal Descents using Singular Perturbation Techniques
Author :
Price, Douglas B.
Author_Institution :
NASA Langley Research Center, Hampton, Virginia
Keywords :
Aerospace control; Aircraft; Control theory; Cost function; Delay; Feedback control; Fuels; NASA; Optimal control; Perturbation methods;
Conference_Titel :
American Control Conference, 1984
Conference_Location :
San Diego, CA, USA
