无人机系统路线图 Unmanned Aircraft Systems Roadmap(198)

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The first area is the development of an Autonomous UAV Mission System (AUMS) for Vertical Takeoff and Landing UA.  The goal of the system is to allow a UA to be launched, recovered, and refueled by a host or stand-alone platform in order to provide force extension through autonomous aerial response.  The recovery capability will be an integration of vision technologies from Carnegie Mellon University and the Jet Propulsion Laboratory as well as GPS technology from Geodetics, Inc.  The system will operate with different manned and unmanned vehicles and will use the JAUS protocol and the SSC-SD MOCU command and control interface.  AUMS may be modified for use by multiple ground and air platforms.  
Some of the near-term UA missions include reconnaissance, RF communications relays, overhead visual GPS augmentation, surveillance, psychological operations, and mine detection.  Future uses include target designation and payload dispersal (i.e., submunitions, ThrowBots, sensors).  Other benefits are seen in the
APPENDIX J – UNMANNED GROUND VEHICLES
Page J-9

UAS ROADMAP 2005

mission flexibility that allows the UA to be launched from one type of system and captured by another (i.e., launched from an UMV and recovered by a HMMVW).  The decrease in time and personnel required to refuel a UA between mission operations leads to an increase in the number of missions a UA can complete in a given period of time.
The second area of development, JAUS-compliant UA, compliments the AUMS project and is producing its own results. SSC-SD is establishing partnerships with Allied Aerospace, Northrop Grumman, Tyndall Air Force Research Laboratory (AFRL), Idaho National Engineering and Environmental Laboratory (INEEL) and Rotomotion, LLC, to develop JAUS VTOL UA platforms.  These platforms will not only be used in the AUMS development, but will also be used for experiments, demonstrations and testing involving UGV-UA cooperation concepts.  The table below lists some of their characteristics. 
The third area of development is UGV-UA collaboration behaviors.  Several application areas that will be explored include:  (1) countermine operations, (2) IED detection, (3) precision targeting using aerial sensors, (4) CBRN contamination, (5) meteorological sensors, (6) communication relays and (7) ThrowBot delivery to areas outside range of manual deployment.  SSC-SD will partner with other government agencies and industry to conduct experiments and demonstrations.  

Allied Aerospace Rotomotion Twin
Yamaha RMAX Type II
iSTAR
Characteristics of Possible Aircraft:
Allied Aerospace iSTAR Ducted Fan  Yamaha RMAX Helicopter  Rotomotion Twin Helicopter 
Size  44” H x 29” W  12’ x 2’ x 3.5’  64” x 20” x 25” 
Main Rotor Diameter  10 ft  72 in 
Tail Rotor Diameter  21 in  14 in 
　
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