Results 81 to 90 of about 32,703 (206)

A24 Direct Yaw Moment Control with EV Kart

open access: yesThe Proceedings of the Symposium on the Motion and Vibration Control, 2005
Kensuke KOBAYASHI   +2 more
openaire   +2 more sources

Pterodactyl: Development and Comparison of Control Architectures for a Mechanically Deployed Entry Vehicle [PDF]

open access: yes
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

open access: yesAdvances in Mechanical Engineering
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

Trajectory Tracking and Stability Control of Distributed-Drive Heavy Trucks on High-Speed Curves with Large Curvature

open access: yesWorld Electric Vehicle Journal
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]

open access: yes
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]

open access: yes
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

The development and application of aerodynamic uncertainties: And flight test verification for the space shuttle orbiter [PDF]

open access: yes
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]

open access: yes, 2008
Benton, Michael J.   +5 more
core   +1 more source

Design criteria for flight evaluation. Monograph 4 - Control system evaluation [PDF]

open access: yes
Methods and analyses for flight evaluation of control systems for multistage launch ...
Sealander, C. E., Zamos, L.
core   +1 more source

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