| contributor author | ARMY - MI - Aviation & Missile Command | |
| date accessioned | 2017-09-04T16:47:24Z | |
| date available | 2017-09-04T16:47:24Z | |
| date copyright | 07/17/1995 | |
| date issued | 1995 | |
| identifier other | WFCZDAAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;query=autho1826AF679D40527369727A00D52FAB6A0Facilities%20Engineering%20Command%226EFDEC9FCD/handle/yse/110754 | |
| description abstract | ![LOGO]()
This handbook is for guidance only. Do not cite this document as a requirement. | |
| language | English | |
| title | MIL-HDBK-1211 | num |
| title | MISSILE FLIGHT SIMULATION PART ONE SURFACE-TO-AIR MISSILES | en |
| type | standard | |
| page | 246 | |
| status | Active | |
| tree | ARMY - MI - Aviation & Missile Command:;1995 | |
| contenttype | fulltext | |
| subject keywords | Aerodynamic forces | |
| subject keywords | Boresight axis | |
| subject keywords | Coordinate system transformation | |
| subject keywords | Coordinate systems | |
| subject keywords | Coriolis acceleration | |
| subject keywords | Degrees of freedom | |
| subject keywords | Equations of motion | |
| subject keywords | Euler angles | |
| subject keywords | Forces and moments | |
| subject keywords | Guidance and control | |
| subject keywords | Mach number | |
| subject keywords | Miss distance | |
| subject keywords | Missile flight path | |
| subject keywords | Missile-target geometry | |
| subject keywords | Moments of inertia | |
| subject keywords | Newton's laws of motion | |
| subject keywords | Propulsion | |
| subject keywords | Reynold's number | |
| subject keywords | Rocket motor | |
| subject keywords | Rotational equations | |
| subject keywords | Scene generation | |
| subject keywords | Target flight path | |
| subject keywords | Target model | |
| subject keywords | Translational equations | |
| subject keywords | Validation | |
درباره ما