Abstract
The integration of flight and propulsion control is an emerging technology that has the potential to offer significant improvements in the mission capabilities of future aircraft systems. Both increased efficiency as well as extended flight and maneuver envelopes have already been demonstrated. There are two main areas of research required to realize fully the benefits of integrating flight and propulsion control. The first is the development of hardware that allows the use of engine air to produce forces and moments about the vehicle axes suitable for high bandwidth attitude control. Thrust vectoring schemes, lift augmentation schemes and direct force/moment control schemes are potential concepts. The second research area is the development of a design approach that will yield integrated control laws.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
