"Design of a multi-vectored thrust aerostat with a reconfigurable control system." Aerosp. Sci. Technol. 53: 95-102. https://doi.org/10.1016/j.ast.2016.03.011.CHEN L, DUAN D P, SUN D S. Design of a multi-vectored thrust aerostat with a reconfigurable control system [J]. Aerospace ...
Design of optimal trajectory transition controller for thrust- vectored V/STOL aircraft. Sci China Inf Sci, 2021, 64(3): 139201, https://doi.org/10.1007/s11432-018-9582-6 Dear editor, In recent years, vertical and/or short take-off and landing (V/STOL) aircraft have attracted much ...
A new approach into design sensitivity studies has been developed, for ease of understanding, to estimate how small changes in the specification would affect a thrust-vectored civil transport aircraft. The equations are linearised and this produces relatively simple relations between the various ...
Thrust-vectoredtail-sitterreconfigurable wingunconventional UAVIn this paper, we present the development of a reconfigurable hybrid unmanned aerial vehicle (UAV): U-Lion [Ang et al., 11th IEEE Int. Conf. Control Automation (ICCA), pp. 750u2013755]. U-Lion is a small-scale UAV that is ...
Design of optimal trajectory transition controller for thrust-vectored V/STOL aircrafttransitionthrustoptimalDear editor,In recent years,vertical and/or short take-off and landing(V/STOL)aircraft have attracted much attention because they combine the efficiency of fixed-wing vehicles with the flexibili...
Design of optimal trajectory transition controller for thrust-vectored V/STOL aircraftoptimalthrusttransitionDear editor,In recent years, vertical and/or short take-off and landing(V/STOL) aircraft have attracted much attention because they combine the efficiency of fixed-wing vehicles with the ...
For the first design, to compensate for uncertainties and also incoming disturbances to the system, a new backstepping fast terminal sliding mode control (BFTSMC) is derived. At the second design, to estimate the upper bound value of the lumped uncertainty in the BFTSMC, an adaptive rule is ...
The essentially nonlinear five-dimensional mathematical model of the longitudinal flight dynamics of a thrust-vectored aircraft in a wing-body coordinate system with two controls, namely, the angular deflections of a movable horizontal stabilizer and a turbojet engine nozzle, is investigated. The core...
Design and Control Strategies of Multirotors with Horizontal Thrust-Vectored PropellersWith the growing adoption of Unmanned Aerial Vehicles (UAVs) in industrial and commercial sectors, the limitations of traditional under-actuated multirotors are becoming increasingly evident, particularly in manipulation ...
For the thrust experiment, the deflection angle of the vectoring nozzle is set to be zero, meaning the nozzle axis is aligned with the engine axis. During the experiment, the rotor speed is fixed at a constant value and the corresponding thrust is measured at the steady state. The rotor ...