DID YOU KNOW? DTIC has over 3.5 million final reports on DoD funded research, development, test, and evaluation activities available to our registered users. Click
HERE to register or log in.
Accession Number:
ADA289271
Title:
Advanced Formation Flight Control.
Descriptive Note:
Master's thesis,
Corporate Author:
AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OH SCHOOL OF ENGINEERING
Report Date:
1994-12-01
Pagination or Media Count:
145.0
Abstract:
In this thesis, the formation flight control problem is continued from four previous theses. Automatic formation flight involves controlling multiple aircraft equipped with standard Mach-hold, altitude hold, and heading-hold autopilots to maintain a desired distance from a lead aircraft or rabbit. Changes in the rabbits states are treated as disturbances to the system and rejected. Previous research is advanced in the following areas Higher-order aircraftautopilot models are included into the design and a new feedback control law is employed, resulting in more accurate simulations. An energy tracking scheme is developed and is shown to reduce wing aircraft energy excursions. Finally, the formation hold autopilot is modified to allow the wing aircraft to orbit a stationary reference point on the earth at a desired range, airspeed, and altitude. The importance of the disturbance rejection capability of the controller is demonstrated through comparisons of linearized model predictions with nonlinear simulations. The design tradeoffs between performance and robustness are emphasized.
Distribution Statement:
APPROVED FOR PUBLIC RELEASE