columbus · Control Systems Theory Applied to the Re-Entry of Aerospace Vehicles

Control Systems Theory Applied to the Re-Entry of Aerospace Vehicles - II

Title: Control Systems Theory Applied to the Re-Entry of Aerospace Vehicles - II
Date: 1964
Index Abstract: Coming Soon
Photo Quality: Not Needed
Report Number: FDL TDR 64-48 Part 1
Creator: Kishi, F. H.
Corporate Author: University of California
Laboratory: AF Flight Dynamics Laboratory
Extent: 164
Identifier: AD0607440
Access Rights: OTS
Distribution Classification: 1
Contract: AF 33(657)-11477
DoD Project: 8225
DoD Task: 822501
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
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.
Report Availability: Full text available
Date Issued: 1964-08
Provenance: Lockheed Martin Missiles & Fire Control
Type: report
Format: 1 online resource