Yaw stabilization of landing craft
, 1966 The purpose of this work was to investigate the application of pump jet propulsion and yaw angle stabilization for a landing craft going through the surf. Linear theory was used throughout the analysis of the control problem. The stability indices and derivatives were determined in part by experiment and the remainder by analytic techniques.
openaire +1 more source
Low-speed wind-tunnel investigation of the flight dynamic characteristics of an advanced turboprop business/commuter aircraft configuration [PDF]
An investigation was conducted to determine the low-speed flight dynamic behavior of a representative advanced turboprop business/commuter aircraft concept. Free-flight tests were conducted in the NASA Langley Research Center's 30- by 60-Foot Tunnel.
Coe, Paul L., Jr. +2 more
core +1 more source
ActuatorsDistributed drive vehicles provide enhanced actuation flexibility, making longitudinal–lateral coordinated stability control essential for improving vehicle handling and safety under complex driving conditions.
Jiansen Yang +5 more
doaj +1 more source
Advanced piloted aircraft flight control system design methodology. Volume 2: The FCX flight control design expert system [PDF]
The development of a comprehensive and electric methodology for conceptual and preliminary design of flight control systems is presented and illustrated.
Mcruer, Duane T., Myers, Thomas T.
core +1 more source
Unified results of several analytical and experimental studies of helicopter handling qualities in visual terrain flight [PDF]
The studies were undertaken to investigate the effects of rotor design parameters, interaxis coupling, and various levels of stability and control augmentation on the flying qualities of helicopters performing low-level, terrain-flying tasks in visual ...
Chen, R. T. N.
core +1 more source
Unsteady aerodynamic analysis of space shuttle vehicles. Part 4: Effect of control deflections on orbiter unsteady aerodynamics [PDF]
The unsteady aerodynamics of the 040A orbiter have been explored experimentally. The results substantiate earlier predictions of the unsteady flow boundaries for a 60 deg swept delta wing at zero yaw and with no controls deflected.
Ericsson, L. E., Reding, J. P.
core +1 more source
Flight control systems properties and problems, volume 1 [PDF]
This volume contains a delineation of fundamental and mechanization-specific flight control characteristics and problems gleaned from many sources and spanning a period of over two decades.
Johnston, D. E., Mcruer, D. T.
core +1 more source
Trajectory Tracking and Yaw Stability Control for Electric Vehicles Based on LTV-MPC
Kongzhi Yu Xinxi JishuThis study focuses on Linear Time-varying Model-based Predictive Control (LTV-MPC) to support real-time trajectory tracking and yaw stability control for distributed drive electric vehicles (DDEV) under steering conditions.
GAO Zhenfei
doaj
Latency-aware attitude control of underactuated quadrotor UAVs using barrier Lyapunov and fuzzy Padé approximation. [PDF]
Sci RepAbro GEM, Memon SA, Hoshu AA, Saeed N.
europepmc +1 more source
An Improved Robust ESKF Fusion Positioning Method with a Novel UWB-VIO Initialization. [PDF]
Sensors (Basel)Wang C +7 more
europepmc +1 more source