DocumentCode
488495
Title
Time-Optimal Aircraft Pursuit-Evasion with A Weapon Envelope Constraint
Author
Menon, P.K.A. ; Duke, E.L.
Author_Institution
School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, GA; Member AIAA, Mail Stop 210-9, NASA Ames Research center, Moffett Field, CA-94035.
fYear
1990
fDate
23-25 May 1990
Firstpage
2337
Lastpage
2342
Abstract
Optimal pursuit-evasion problem between two aircraft including nonlinear point-mass vehicle models and a realistic weapon envelope is analyzed. Using a linear combination of flight time and the square of the vehicle acceleration as the performance index, closed form solution is obtained in nonlinear feedback form. Due to its modest computational requirements, this guidance law useful for on-board real-time implementation.
Keywords
Acceleration; Aircraft; Computer vision; Feedback; Gravity; NASA; Navigation; Performance analysis; Vehicles; Weapons;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1990
Conference_Location
San Diego, CA, USA
Type
conf
Filename
4791146
Link To Document