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 inNonlinear dynamics Vol. 94; no. 3; pp. 2205 - 2218
Main Author Nanjangud, Angadh
Format Journal Article
LanguageEnglish
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.
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
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10.2514/3.3544
10.2514/2.3586
10.2514/1.59686
10.2514/1.62695
10.1115/1.2896031
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Copyright The Author(s) 2018
Copyright Springer Science & Business Media 2018
Nonlinear Dynamics is a copyright of Springer, (2018). All Rights Reserved. © 2018. This work is published under http://creativecommons.org/licenses/by/4.0 (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.
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– notice: Nonlinear Dynamics is a copyright of Springer, (2018). All Rights Reserved. © 2018. This work is published under http://creativecommons.org/licenses/by/4.0 (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.
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Mass variation
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A Nanjangud (4485_CR16) 2017; 64
D Javorsek (4485_CR21) 2000; 37
S Djerassi (4485_CR6) 1998; 21
4485_CR23
JCVD Ha (4485_CR15) 2005; 28
L Cveticanin (4485_CR10) 2007; 55
FO Eke (4485_CR13) 2004; 71
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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. Sci.200048435448
– reference: CochranJEJrKangJYNonlinear stability analysis of the attitude motion of a spin-stabilized upper stageAdv. Astronaut. Sci.1991751345364
– reference: JavorsekDLonguskiJMVelocity pointing errors associated with spinning thrusting spacecraftJ. Spacecr. Rockets200037335936510.2514/2.3586
– reference: CveticaninLDjukicDMotion of body with discontinual mass variationNonlinear Dyn.200852324926110.1007/s11071-007-9275-5(2007)1170.70383
– reference: EkeFOWangS-MAttitude behavior of a variable mass cylinderJ. Appl. Mech.199562493594010.1115/1.2896025
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Snippet 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...
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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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