Geometry of motion and nutation stability of free axisymmetric variable mass systems
In classical mechanics, the ‘geometry of motion’ refers to a development to visualize the motion of freely spinning bodies. In this paper, such an approach of studying the rotational motion of axisymmetric variable mass systems is developed. An analytic solution to the second Euler angle characteriz...
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Published in | Nonlinear dynamics Vol. 94; no. 3; pp. 2205 - 2218 |
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Main Author | |
Format | Journal Article |
Language | English |
Published |
Dordrecht
Springer Netherlands
01.11.2018
Springer Nature B.V |
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Abstract | In classical mechanics, the ‘geometry of motion’ refers to a development to visualize the motion of freely spinning bodies. In this paper, such an approach of studying the rotational motion of axisymmetric variable mass systems is developed. An analytic solution to the second Euler angle characterizing nutation naturally falls out of this method, without explicitly solving the nonlinear differential equations of motion. This is used to examine the coning motion of a free axisymmetric cylinder subject to three idealized models of mass loss and new insight into their rotational stability is presented. It is seen that the angular speeds for some configurations of these cylinders grow without bounds. In spite of this phenomenon, all configurations explored here are seen to exhibit nutational stability, a desirable property in solid rocket motors. |
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AbstractList | In classical mechanics, the ‘geometry of motion’ refers to a development to visualize the motion of freely spinning bodies. In this paper, such an approach of studying the rotational motion of axisymmetric variable mass systems is developed. An analytic solution to the second Euler angle characterizing nutation naturally falls out of this method, without explicitly solving the nonlinear differential equations of motion. This is used to examine the coning motion of a free axisymmetric cylinder subject to three idealized models of mass loss and new insight into their rotational stability is presented. It is seen that the angular speeds for some configurations of these cylinders grow without bounds. In spite of this phenomenon, all configurations explored here are seen to exhibit nutational stability, a desirable property in solid rocket motors. |
Author | Nanjangud, Angadh |
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Cites_doi | 10.2514/6.1986-2271 10.1007/s11071-007-9275-5(2007) 10.2514/3.20837 10.1007/s11071-008-9362-2 10.1007/BF03546265 10.1115/1.2896025 10.2514/3.21525 10.2514/2.4556 10.2514/1.A33152 10.1115/1.1653738 10.1007/s40295-016-0099-8 10.2514/6.1985-1382 10.2514/3.29262 10.1016/j.ast.2018.03.003 10.2514/3.3544 10.2514/2.3586 10.2514/1.59686 10.2514/1.62695 10.1115/1.2896031 |
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References_xml | – reference: WangS-MEkeFORotational dynamics of axisymmetric variable mass systemsJ. Appl. Mech.199562497097410.1115/1.2896031 – reference: EkeFOMaoT-CMorrisMJFree attitude motions of a spinning body with substantial mass lossJ. Appl. Mech.200471219019410.1115/1.1653738 – reference: Nanjangud, A.: On the rotational dynamics of variable mass systems. Ph.D. dissertation, University of California, Davis (2016) – reference: BarkleyRJNewtonRRGrossGLMathematical Theory of Rocket Flight1947New YorkMcGraw-Hill – reference: ReiterGThomsonWJet damping of a solid rocket-theory and flight resultsAIAA J.19653413417 – reference: KaplanMHModern Spacecraft Dynamics and Control1976New YorkWiley – reference: OrACRotor-pendulum model for the perigee assist module nutation anomalyJ. Guid. Control Dyn.199215229730310.2514/3.20837 – reference: ThomsonWTEquations of motion for the variable mass systemAIAA J.19664766768 – reference: BanerjeeAKDynamics of a variable-mass, flexible-body systemJ. Guid. Control Dyn.20002350150810.2514/2.4556 – reference: WebsterEActive Nutation Control for Spinning Solid Motor Upper Stages1985Monterey, CAAmerican Institute of Aeronautics and Astronautics10.2514/6.1985-1382 – reference: NanjangudAEkeFOLagrange’s equations for rocket-type variable mass systemsInt. Rev. Aerosp. Eng.201255256260 – reference: ThomsonWTIntroduction to Space Dynamics1986New YorkDover – reference: SnyderVWWarnerGGA re-evaluation of jet dampingJ. Spacecr. Rockets1968536436610.2514/3.29262 – reference: HalsmerDMMingoriDLNutational stability and passive control of spinning rockets with internal mass motionJ. Guid. Control Dyn.19951851197120310.2514/3.21525 – reference: DjerassiSAlgorithm for simulation of motions of variable-mass systemsJ. Guid. Control Dyn.199821427434 – reference: Mingori, D., Yam, Y.: Nutational Stability of a Spinning Spacecraft with Internal Mass Motion and Axial Thrust. AIAA Paper 86-2271 AIAA Astrodynamics Conference Proceedings (Williamsburg, VA), pp. 367-375. AIAA, Washington, DC (1986) – reference: HuPRenGMultibody dynamics of flexible liquid rockets with depleting propellantJ. Guid. Control Dyn.2013361840184910.2514/1.59686 – reference: HaJCVDJanssensFLJet-damping and misalignment effects during solid rocket motor burnJ. Guid. Control Dyn.200528412420 – reference: MartinKMLonguskiJMVelocity pointing error reduction for spinning, thrusting spacecraft via heuristic thrust profilesJ. Spacecr. Rockets20155241268127210.2514/1.A33152 – reference: CveticaninLDynamics of body separationanalytical procedureNonlinear Dyn.2007553269278239085910.1007/s11071-008-9362-2 – reference: MaoTCEkeFOAttitude dynamics of a torque-free variable mass cylindrical bodyJ. Astronaut. 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SubjectTerms | Angular speed Automotive Engineering Axisymmetric bodies Classical Mechanics Configurations Coning motion Control Cylinders Dynamical Systems Engineering Equations of motion Euler angles Exact solutions Mechanical Engineering Motion stability Nonlinear differential equations Nonlinear equations Nutation Original Paper Rocket engines Solid propellant rocket engines Variable mass systems Vibration |
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Title | Geometry of motion and nutation stability of free axisymmetric variable mass systems |
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