Control Systems Theory Applied to the Re-Entry of Aerospace Vehicles - II
Report Number: FDL TDR 64-48 Part 1
Author(s): Kishi, F. H.
Corporate Author(s): University of California
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-08
Pages: 164
Contract: AF 33(657)-11477
DoD Project: 8225
DoD Task: 822501
Identifier: AD0607440
Abstract:
In an effort to bridge the gap between theory and practice, the re-entry problem area is chosen to apply advanced control techniques. This problem area affords many separate areas where theory could be applied. This volume is separated into two parts: Part 1 describes digital computer controlled adaptive processes which can be employed for the flight path control problem; i.e., control of a vehicle about a predetermined trajectory (optimal or otherwise). In Part 2 optimal re-entry trajectories are determined.
Provenance: Lockheed Martin Missiles & Fire Control
Author(s): Kishi, F. H.
Corporate Author(s): University of California
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-08
Pages: 164
Contract: AF 33(657)-11477
DoD Project: 8225
DoD Task: 822501
Identifier: AD0607440
Abstract:
In an effort to bridge the gap between theory and practice, the re-entry problem area is chosen to apply advanced control techniques. This problem area affords many separate areas where theory could be applied. This volume is separated into two parts: Part 1 describes digital computer controlled adaptive processes which can be employed for the flight path control problem; i.e., control of a vehicle about a predetermined trajectory (optimal or otherwise). In Part 2 optimal re-entry trajectories are determined.
Provenance: Lockheed Martin Missiles & Fire Control