Close Air Support Missile Guidance and Control Study. Volume I. Six- Degree-of-Freedom Simulation
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| Název: | Close Air Support Missile Guidance and Control Study. Volume I. Six- Degree-of-Freedom Simulation |
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| Autoři: | Mahig, J. |
| Přispěvatelé: | FLORIDA UNIV GAINESVILLE DEPT OF MECHANICAL ENGINEERING |
| Zdroj: | DTIC AND NTIS |
| Rok vydání: | 1971 |
| Sbírka: | Defense Technical Information Center: DTIC Technical Reports database |
| Témata: | Computer Programming and Software, Test Facilities, Equipment and Methods, Air- and Space-launched Guided Missiles, COMPUTER PROGRAMS, GUIDED MISSILE SIMULATORS, SIMULATION, EQUATIONS OF MOTION, GUIDED MISSILE TRAJECTORIES, CLOSE SUPPORT, PASSIVE SYSTEMS, LASERS, TACTICAL AIR SUPPORT, HOMING DEVICES, ACTUATORS, SUBROUTINES, AIR TO AIR MISSILES, AUTOMATIC PILOTS, AIR TO SURFACE MISSILES, SOLID PROPELLANT ROCKET ENGINES, AERODYNAMICS, MISS DISTANCE, SEMIACTIVE GUIDANCE, SIX DEGREE OF FREEDOM SIMULATORS |
| Popis: | This report describes in detail a six-degree-of-freedom program which can be used to determine the trajectory and miss distance of a missile system. The options for the program are such as to permit variation of the aerodynamics, seeker, autopilot actuator and missile motor performance for the purpose of accurately simulating a given missile design and evaluating the effects of changes in system parameters. Sufficient detail has been included in the text in order to minimize the users' effort needed to know how to update or modify the program for his purposes. ; See also Volume 2, AD892612. |
| Druh dokumentu: | text |
| Popis souboru: | text/html |
| Jazyk: | English |
| Relation: | http://www.dtic.mil/docs/citations/AD0892611 |
| Dostupnost: | http://www.dtic.mil/docs/citations/AD0892611 http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=AD0892611 |
| Rights: | APPROVED FOR PUBLIC RELEASE |
| Přístupové číslo: | edsbas.83693D3E |
| Databáze: | BASE |
Nájsť tento článok vo Web of Science | Abstrakt: | This report describes in detail a six-degree-of-freedom program which can be used to determine the trajectory and miss distance of a missile system. The options for the program are such as to permit variation of the aerodynamics, seeker, autopilot actuator and missile motor performance for the purpose of accurately simulating a given missile design and evaluating the effects of changes in system parameters. Sufficient detail has been included in the text in order to minimize the users' effort needed to know how to update or modify the program for his purposes. ; See also Volume 2, AD892612. |
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