AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR
SAE International
1. SCOPE
2. REFERENCES
3. NA: USED FOR DATA OR RECOMMENDATIONS
THAT ARE NOT AVAILABLE RECOMMENDATIONS
4. VERIFICATION AND VALIDATION
5. NOTES
APPENDIX A - RECOMMENDATION APPLICABILITY
BY VMS TYPE
Determines recommended practices for the specification of general performance, design, test, development, and quality assurance requirements for the flight control related functions of the Vehicle Management Systems (VMS) of military Unmanned Aircraft (UA), the airborne element of Unmanned Aircraft Systems (UAS), as defined by ASTM F 2395-07.
| Document Type | Standard |
| Status | Current |
| Publisher | SAE International |
| Committee | A-6 |
