Abstract
Nomenclature CD = drag coefficient CL = lift coefficient D = drag E = energy g = acceleration due to gravity H = Hamiltonian h = altitude J performance criterion K = lift dependent drag factor (CD = CDo + KCl) L = lift 772 = mass myexponent denoting the dependence of thrust specific fuel consumption on speed P = propulsive power, TV S = reference area S = switching function T = thrust F = speed x = horizontal coordinate y state variables vector 7 = flight path angle 6 = throttle setting X = Lagrange multiplier v — specific fuel consumption related to propulsive power p = atmospheric density a = specific fuel consumption related to thrust
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.
