Application of the Estimation-Before-Modeling (EBM) System Identification Method to the High Angle of Attack/Sideslip Flight of the T-2c Jet Trainer Aircraft. Volume 1. Executive Summary

doi 10.21236/ada080025
Full Text
Abstract

Available in full text

Date
Authors
Publisher

Defense Technical Information Center

Related search

Application of Bifurcation Theory to the High-Angle-Of-Attack Dynamics of the F-14

Journal of Aircraft
Aerospace Engineering
1994English

Nonlinear Stabilizing Control of High Angle of Attack Flight Dynamics

1989English

Application of Recursive Least Square Algorithm on Estimation of Vehicle Sideslip Angle and Road Friction

Mathematical Problems in Engineering
MathematicsEngineering
2010English

Evaluation of the 175/40 Initial Entry Rotary Wing Flight Training Program. Volume I. Executive Summary

1979English

Vulnerability Methodology and Protective Measures for Aircraft Fire and Explosion Hazards. Volume 1. Executive Summary

1986English

Development of a Method for Establishing Resurfacing Priorities for the Pavement Management in Indiana: Volume 1, Executive Summary

1984English

A Vision Based Method for Aircraft Approach Angle Estimation

Ruan Jian Xue Bao/Journal of Software
Software
2006English

Advanced Avionics Computer Architecture. Volume 1. Executive Summary.

1985English

In-Flight Flow Visualization Results From the X-29a Aircraft at Highangles of Attack

1992English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2024 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy