Analyzing the spatial motion of a rigid body subjected to constant body-fixed torques and gyrostatic moment

被引:13
|
作者
Amer, T. S. [1 ]
El-Kafly, H. F. [2 ]
Elneklawy, A. H. [3 ]
Galal, A. A. [4 ]
机构
[1] Tanta Univ, Fac Sci, Dept Math, Tanta 31527, Egypt
[2] Tanta Higher Inst Engn & Technol, Tanta, Egypt
[3] Kafrelsheikh Univ, Fac Sci, Dept Math, Kafr Al Sheikh 33516, Egypt
[4] Tanta Univ, Fac Engn, Engn Phys & Math Dept, Tanta 31734, Egypt
关键词
Nonlinear dynamics; Rigid body; Constant torques; Gyrostatic moment; Stability analysis; STATIONARY ORBIT; EQUILIBRIUM ATTITUDE; ANALYTIC SOLUTIONS; SPACECRAFT; STABILITY; SATELLITE; ROTATION; POINT;
D O I
10.1038/s41598-024-55964-z
中图分类号
O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];
学科分类号
07 ; 0710 ; 09 ;
摘要
This paper aims to explore the rotatory spatial motion of an asymmetric rigid body (RB) under constant body-fixed torques and a nonzero first component gyrostatic moment vector (GM). Euler's equations of motion are used to derive a set of dimensionless equations of motion, which are then proposed for the stability analysis of equilibrium points. Specifically, this study develops 3D phase space trajectories for three distinct scenarios; two of them are applied constant torques that are directed on the minor and major axes, while the third one is the action of applied constant torque on the body's middle axis. Novel analytical and simulation results for both scenarios of constant torque applied along the minor and middle axes are provided in the context of separatrix surfaces, equilibrium manifolds, periodic or non-periodic solutions, and periodic solutions' extreme. Concerning the scenario of a directed torque on the major axis, a numerical solution for the problem is presented in addition to a simulation of the graphed results for the angular velocities' trajectories in various regions. Moreover, the influence of GM is examined for each case and a full modeling for the body's stability has been present. The exceptional impact of these results is evident in the development and assessment of systems involving asymmetric RBs, such as satellites and spacecraft. It may serve as a motivating factor to explore different angles within the GM in similar cases, thereby influencing various industries, including engineering and astrophysics applications.
引用
收藏
页数:22
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