PREDICTION OF TRAJECTORY OF SPACE VEHICLE UNDER DISCRETE CONTROL,
Abstract
Spacecraft trajectories are predicted using the principle of maximum probability. Perturbations are Gaussian random functions. It is desired to change the controlling action, depending upon measured values, so as to reduce probable deviations of elements of the 'final miss' vector to a minimum.
Document Details
- Document Type
- Technical Report
- Publication Date
- May 25, 1965
- Accession Number
- AD0615859
Entities
People
- V. A. Yaroshevskii
Organizations
- National Air and Space Intelligence Center