Study on Initial Disturbance of Airborne Missile’s Horizontal Backward Derailment under Continuous Gust
This paper studies the effect of continuous gusts on the initial disturbance of the airborne missile’s horizontal backward derailment on large transport aircraft. The longitudinal fluctuation of the airborne launching platform under continuous gust was obtained with different calculation methods, an...
Saved in:
Main Authors: | Xiao Pan, Yi Jiang, Xinlin Wei, Mingjun Li |
---|---|
Format: | Article |
Language: | English |
Published: |
Wiley
2019-01-01
|
Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2019/5620124 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Influence of External Factors on Airborne Missile’s Horizontal Backward Launching
by: Xiao Pan, et al.
Published: (2021-01-01) -
Horizontal Backward Launch Dynamics Modeling and Analysis
by: Liangyu Zhao, et al.
Published: (2019-01-01) -
ANALYSIS AND TEST METHODS OF SUSPENSION STRUCTURE OF AIRBORNER MISSILE
by: SONG Lei, et al.
Published: (2019-01-01) -
The Gust Factor Models Involving Wind Speed and Temperature Profiles for Wind Gust Estimation
by: Haichuan Hu, et al.
Published: (2024-01-01) -
A Robust Control for an Aerial Robot Quadrotor under Wind Gusts
by: Li Ding, et al.
Published: (2018-01-01)