Propulsion and launching analysis of variable-mass rockets by analytical methods
Propulsion and Power Research, 2013 In this study, applications of some analytical methods on nonlinear equation of the launching of a rocket with variable mass are investigated. Differential transformation method (DTM), homotopy perturbation method (HPM) and least square method (LSM) were
D.D. Ganji +4 more
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Simulation Model for Hardware-in-the-Loop Tests of the ILR-33 AMBER Rocket Control System [PDF]
SensorsIn this paper, an advanced flight simulation model of the ILR-33 AMBER rocket is shown. The model is designed for Hardware-in-the-Loop (HiL) tests of the rocket control system.
Dawid Cieśliński +4 more
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Heliyon, 2023 The geometry under consideration for this flow problem, namely paraboloid surface is similar to aircraft and car bonnet, bullet shape, front shape of submarine, rockets and these types of are useful in manufacturing of formula F1 cars and airplanes.
Muhammad Awais, T. Salahuddin
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Rotary Motion of Variable Mass Cylinder [PDF]
مجله مدل سازی در مهندسی, 2009 In this paper with the use of theory of variable mass systems and dynamic analysis, rotary motion of variable mass cylinder has been evaluated. Effects of angular rates, the methods of mass reduction and propellant burn, the shape and measurement of ...
سعدالدین +3 more
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Attitude Dynamics of a Spinning Rocket with Internal Fluid Whirling Motion [PDF]
INCAS Bulletin, 2014 This paper evaluates the impact that helical motion of fluid products of combustion within the combustion chamber of a rocket can have on the attitude dynamics of rocket systems.
Marius Ionut MARMUREANU, Ion FUIOREA
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Equations of motion for the variable mass flow-variable exhaust velocity rocket [PDF]
Astrodynamics Conference, 1972 An equation of motion for a one dimensional rocket is derived as a function of the mass flow rate into the acceleration chamber and the velocity distribution along the chamber, thereby including the transient flow changes in the chamber. The derivation of the mass density requires the introduction of the special time coordinate.
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Attitude stability and altitude control of a variable-geometry Earth-orbiting solar sail [PDF]
, 2016 A variable-geometry solar sail for on-orbit altitude control is investigated. It is shown that, by adjusting the effective area of the sail at favorable times, it is possible to influence the length of the semi-major axis over an extended period of time.
Ceriotti, Matteo +2 more
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General motion of a variable-mass flexible rocket with internal flow [PDF]
Journal of Spacecraft and Rockets, 1970 This paper consists of two parts. In the first part a new and general formulation of the dynamical problems associated with the powered flight of variable-mass , flexible rockets with internal gas flow is presented. The formulation comprises six ordinary differential equations for the rigid-body motion and three partial differential equations for the ...
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Hybrid fuzzy sliding mode control for motorised space tether spin-up when coupled with axial and torsional oscillation [PDF]
, 2010 A specialised hybrid controller is applied to the control of a motorised space tether spin-up space coupled with an axial and a torsional oscillation phenomenon.
Cartmell, M., Chen, Y.
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Modeling for Active Control of Combustion and Thermally Driven Oscillations [PDF]
, 1991 Organized oscillations excited and sustained by high densities of energy release in combustion chambers have long caused serious problems in development of propulsion systems.
Culick, F. E. C. +3 more
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