A24 Direct Yaw Moment Control with EV Kart
Kensuke KOBAYASHI +2 more
openaire +2 more sources
Pterodactyl: Development and Comparison of Control Architectures for a Mechanically Deployed Entry Vehicle [PDF]
The Pterodactyl project, seeks to advance the current state-of-the-art for entry vehicles by developing novel guidance and control technologies for Deployable Entry Vehicles (DEVs) that can be applied to various entry vehicle configurations.
Barton, Jeffrey D. +3 more
core +1 more source
The direct yaw-moment control based on adaptive fuzzy LQR for distributed drive electric vehicles
This paper introduced a hierarchical control strategy for direct yaw moment (DYC) to enhance the handling and stability of distributed drive electric vehicles (DDEVs) at medium to high speeds. The upper controller entailed a speed-following PI controller
Baohua Wang +3 more
doaj +1 more source
To address the difficulty of balancing trajectory-tracking accuracy and yaw stability for distributed-drive four-axle heavy trucks under high-speed and large-curvature cornering conditions, this paper proposes a hierarchical cooperative control strategy.
Zhi Li, Zhouquan Li, Huawei Wu, Zhen Liu
doaj +1 more source
The effect of yaw on horizontal axis wind turbine loading and performance [PDF]
The Mod-0 100 kW experimental wind turbine was tested to determine the effects of yaw on rotor power, blade loads and teeter response. The wind turbine was operated for extended periods at yaw angles up to 49 deg to define average or mean response to yaw.
Corrigan, R. D. +2 more
core +1 more source
A flight investigation of the wake turbulence alleviation resulting from a flap configuration change on a B-747 aircraft [PDF]
A flight test investigation was conducted to evaluate the effects of a flap configuration change on the vortex wake characteristics of a Boeing 747 (B-747) aircraft as measured by differences in upset response resulting from deliberate vortex encounters ...
Jacobsen, R. A., Short, B. J.
core +1 more source
Rotorcraft linear simulation model. Volume 3: User's manual [PDF]
For abstract, see N78 ...
Reaser, J. S.
core +1 more source
The development and application of aerodynamic uncertainties: And flight test verification for the space shuttle orbiter [PDF]
The approach used in establishing the predicted aerodynamic uncertainties and the process used in applying these uncertainties during the design of the Orbiter flight control system and the entry trajectories are presented.
Cooke, D. R. +4 more
core +1 more source
Aerodynamic characters of the cranial crest in Pteranodon [PDF]
Benton, Michael J. +5 more
core +1 more source
Design criteria for flight evaluation. Monograph 4 - Control system evaluation [PDF]
Methods and analyses for flight evaluation of control systems for multistage launch ...
Sealander, C. E., Zamos, L.
core +1 more source

