Simulation of Launch Dynamics of Aircraft Based on ADAMS and AMESim

ZHAO  Junwei; ZHANG  Jiajun; ZHANG  Cheng; SI  Shicai; QIU  Qunhai

doi:10.15892/j.cnki.djzdxb.2021.05.010

Journal of Projectiles, Rockets, Missiles and Guidance >

2021 , Vol. 41 >Issue 5: 46 - 52

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2021.05.010

Simulation of Launch Dynamics of Aircraft Based on ADAMS and AMESim

ZHAO Junwei ,
ZHANG Jiajun ,
ZHANG Cheng ,
SI Shicai ,
QIU Qunhai

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China Academy of Launch Vehicle Technology, Beijing 100076, China

Received date: 2020-10-10

Online published: 2025-05-30

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Abstract

Based on the joint simulation technology of ADAMS and AMESim, this paper establishes the launch vehicle and aircraft multibody dynamics model in ADAMS software, establishes the launch vehicle hydraulic subsystem model in AMESim, and adopts joint simulation to carry out the dynamic simulation analysis of the launch process of a certain aircraft. After analysis, it is confirmed that the attitude angle and angular velocity of the aircraft are normal after the vehicle is launched out of the box, which meets the control conditions of the attitude control system.

Key words： co-simulation; aircraft; launch; dynamics

Cite this article

ZHAO Junwei , ZHANG Jiajun , ZHANG Cheng , SI Shicai , QIU Qunhai . Simulation of Launch Dynamics of Aircraft Based on ADAMS and AMESim[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2021 , 41(5) : 46 -52 . DOI: 10.15892/j.cnki.djzdxb.2021.05.010

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