Aeroelastic Control-Oriented Modeling of an Airbreathing Hypersonic Vehicle
نویسندگان
چکیده
منابع مشابه
A Velocity-based Lpv Modeling and Control Framework for an Airbreathing Hypersonic Vehicle
This paper focuses on developing a linear parameter varying (LPV) controller for an airbreathing hypersonic vehicle using a velocity-based approach. The design of flight control systems for airbreathing hypersonic vehicles is a highly challenging task due to the unique characteristics of the vehicle dynamics. Motivated by recent results on a velocity-based linearization approach and LPV control...
متن کاملControl Oriented Modeling of 6-DOF Hypersonic Vehicle Dynamics
The derivation of a control-design model (CDM) of the 6-DOF rigid body dynamics of a hypersonic vehicle is presented in this paper. The development of the CDM is based on curve t approximation of the forces and moments on the vehicle, making the model suitable for control design. In order to have an implementable curve t algorithm, the forces and moments have been divided into their components ...
متن کاملBoundary Layer Control for Hypersonic Airbreathing Vehicles
Active and passive methods for tripping hypersonic boundary layers have been examined in NASA Langley Research Center wind tunnels using a Hyper-X model. This investigation assessed several concepts for forcing transition, including passive discrete roughness elements and active mass addition (or blowing), in the 20-Inch Mach 6 Air and the 31-Inch Mach 10 Air Tunnels. Heat transfer distribution...
متن کاملdevelopment and implementation of an optimized control strategy for induction machine in an electric vehicle
in the area of automotive engineering there is a tendency to more electrification of power train. in this work control of an induction machine for the application of electric vehicle is investigated. through the changing operating point of the machine, adapting the rotor magnetization current seems to be useful to increase the machines efficiency. in the literature there are many approaches wh...
15 صفحه اول1 The Use of Energy - State Analysis on a Generic Airbreathing Hypersonic Vehicle
A possible next-generation launch vehicle may be a fully reusable, single-stage-to-orbit (SSTO) aerospacecraft. This class of hypersonic vehicle includes highly integrated airframe and propulsion systems, hence fuel-optimal trajectories are of special interest. Also, since these vehicles are neither conventional aircraft nor rockets, the appropriate approach for trajectory analysis during preli...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
ژورنال
عنوان ژورنال: Journal of Guidance, Control, and Dynamics
سال: 2018
ISSN: 0731-5090,1533-3884
DOI: 10.2514/1.g002777