Certain Problems of Structural Synthesis of Spatial Motion Control Systems for an Orbital Aircraft in the Earth's Atmosphere,
Abstract
A theoretical analysis is given of linear multichannel control systems for vehicles orbiting in the atmosphere of the earth at supersonic velocities. A procedure is developed for obtaining a set of control system structures providing a selection invariance which can be used as a basis for the optimization of such control systems in terms of both quality and simplicity of realization. Equations describing the spatial motion of such vehicles and a graphic mathematical model of these equations are derived in the process. The methods of graph theory are applied in developing the algorithms for constructing such control systems.
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 13, 1970
- Accession Number
- AD0714796
Entities
People
- A. I. Pavlenko
- B. N. Petrov
- N. P. Kolpakova
- V. A. Vasilev
Organizations
- National Air and Space Intelligence Center