Missile Motion Sensitivity to Dynamic Stability Derivatives
Report Number: AEDC TR 80-11
Author(s): Langham, T. F.
Corporate Author(s): ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1980-09-01
Pages: 112
Contract: Laboratory Research - No Contract
DoD Project: None Given
Identifier: ADA089750
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.
Provenance: AFRL/VACA
Author(s): Langham, T. F.
Corporate Author(s): ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1980-09-01
Pages: 112
Contract: Laboratory Research - No Contract
DoD Project: None Given
Identifier: ADA089750
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.
Provenance: AFRL/VACA