columbus · Missile Motion Sensitivity to Dynamic Stability Derivatives

Missile Motion Sensitivity to Dynamic Stability Derivatives

Title: Missile Motion Sensitivity to Dynamic Stability Derivatives
Date: 1980
Index Abstract: Coming Soon
Photo Quality: Not Needed
Report Number: AEDC TR 80-11
Corporate Author: ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date Issued: 1980-09-01
Extent: 112
Identifier: ADA089750
Access Rights: Approved for public release; distribution unlimited.
Distribution Classification: 1
Contract: Laboratory Research - No Contract
DoD Project: None Given
DoD Task: None Given
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Abstract: A dynamic derivative sensitivity study was conducted to demonstrate the importance of dynamic derivatives in missile motion simulation studies. Generalized bank-to-turn and yaw-to-turn missile configurations were used with a six-degree-of-freedom linearized stability program. The effects of various dynamic derivatives on missile stability were investigated in both level and turning flight for several Mach numbers and altitude conditions.
Report Availability: Full text available
Publisher: Arnold Air Force Station, TN : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force
Provenance: AFRL/VACA
Type: report
Format: 1 online resource
Creator: Langham, T. F.