DocumentCode

486022

Title

Feedback Control for Fuel-Optimal Descents using Singular Perturbation Techniques

Author

Price, Douglas B.

Author_Institution

NASA Langley Research Center, Hampton, Virginia

fYear

1984

fDate

6-8 June 1984

Firstpage

198

Lastpage

203

Keywords

Aerospace control; Aircraft; Control theory; Cost function; Delay; Feedback control; Fuels; NASA; Optimal control; Perturbation methods;

fLanguage

English

Publisher

ieee

Conference_Titel

American Control Conference, 1984

Conference_Location

San Diego, CA, USA

Type

conf

Filename

4788376