Aerospace - Vehicle Management Systems - Flight Control Design, Installation and Test of, Military Unmanned Aircraft, Specification Guide For

Standard:
Issued:
  • 2012-12-19
 
  • CURRENT
Publisher:
  • SAE International
Pages:
113
Scope:

This document establishes 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. The document is written for military unmanned aircraft intended for use primarily in military operational areas. The document also provides a foundation for considerations applicable to safe flight in all classes of airspace.

Rationale:

This document is published for the following reasons: a. Address the need for standards and guide documents for Unmanned Aircraft onboard systems. b. Provide recommended practices for the specification of the flight control related functions of military Unmanned Aircraft Vehicle Management Systems. c. Recommend a method for the specification of the appropriate level of flight control capability for an Unmanned Aircraft. d. Address the integration of the flight control functions with all other elements of the vehicle.

History:
Standard Published Revision Status
ARP94910 2012-12-19 Latest Issued
Access
Now
SAE MOBILUS Subscriber? You may already have access.
Buy
Select
Price
List
Download
$76.00
Add
Mail
$76.00
Members save up to 18% off list price.
Grade
If you are currently using this technical report:
Share
HTML for Linking to Page
Page URL

Related Items

Training / Education
2018-04-10
Training / Education
2013-02-20
Technical Paper / Journal Article
2010-10-25