Longitudinal Air-Breathing Hypersonic Vehicle Nonlinear Dynamic Simulation with Different Control Inputs

被引：0
|
作者：
Singh, Ritesh [1 ,2 ]
Prakash, Om [1 ]
Joshi, Sudhir [3 ]
Sharma, Rakesh Chandmal [4 ,5 ]
机构：
[1] Univ Petr & Energy Studies, Dept Aerosp Engn, Dehra Dun, India
[2] Manipal Univ Jaipur, Dept Elect Engn, Jaipur, India
[3] Graph Era Deemed Univ, Dept Environm Sci, Dehra Dun, India
[4] Graph Era Deemed Univ, Dept Mech Engn, Dehra Dun, India
[5] Graph Era Hill Univ Dehradun, Mech Engn Dept, Dehra Dun, India
来源：
SAE INTERNATIONAL JOURNAL OF AEROSPACE | 2024年 / 17卷 / 02期
关键词：
Air-breathing Hypersonic; Vehicle; AHV; Future; Hypersonic Vehicle; Dynamic Simulation; Longitudinal Model; Trim; Simulation; Stability; Bifurcation Method;
D O I：
10.4271/01-17-02-0015
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The air-breathing hypersonic vehicle (AHV) holds the potential to revolutionize global travel, enabling rapid transportation to low-Earth orbit and even space within the next few decades. This study focuses on investigating the nonlinear dynamic simulation, trim, and stability analysis of a threedegrees-of-freedom (3DOF) longitudinal model of a generic AHV for variable control surface deflection, delta e and delta r. A simulation is developed to analyze the burstiness of the AHV's nonlinear longitudinal behavior, considering the complete flight envelope across a wide range of Mach numbers, from M = 0 to 24, for selected stable M. The presented simulation assesses trim analysis and explores the dynamic stability of the AHV through its flight envelope and bifurcation method analysis is carried out to gain insight and validate the dynamic stability using eigen value approach.
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页数：20
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