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- W2043144590 abstract "T article examines several problems related to the control of an interplanetary missile. By an interplanetary missile we mean an apparatus moving outside the limits of the atmosphere. This may be an artificial Earth satellite, a stage of a space rocket, etc. The control system for such a missile must permit it to change the motion of the center of mass of the missile and execute arbitrary rotations about the center of mass; it must also be possible to keep the axis of the missile in a given position. To move the missile about the center of mass, Tsiolkovsky proposed two methods: Creation of a reactive force for which the line of action does not pass through the missile's center of mass, and the use of reactive flywheels. Control of the missile by means of reactive engines can be analyzed relatively simply. However, analysis of the control with the aid of reactive flywheels cannot. For purposes of generalization, let us suppose that the number of stabilizing flywheels in the body of the missile is equal to n. Use of an arbitrary number of flywheels does not introduce any complications in writing the equations of motion. We will consider the positions of the flywheels and the orientations of their axes within the body of the missile as arbitrary, but fixed with respect to time; let us also suppose that the flywheels are statically and dynamically balanced upon their axes; in other words, their axes of rotation are the main central axes of inertia. This assumption is obviously correct for flywheels with axial symmetry." @default.
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- W2043144590 date "1961-11-01" @default.
- W2043144590 modified "2023-10-05" @default.
- W2043144590 title "Some Guidance Problems in Interplanetary Space" @default.
- W2043144590 doi "https://doi.org/10.2514/8.5859" @default.
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