Robotic Aircraft for Public Safety (RAPS)

advertisement

ROBOTIC AIRCRAFT FOR

PUBLIC SAFETY (RAPS)

OVERVIEW

Kirk Kloeppel

4 June 2014

UAS or “DRONE”

2

Introduction

RAPS Purpose

To provide potential users (public, first responder organizations and others) with information needed to make informed decisions on acquiring and deploying SUAS to save lives and protect property

RAPS testing focuses on fire response, search and rescue operations,

HAZMAT response, border security, natural disasters, and law enforcement

RAPS provides a unique ‘Consumer Reports’ data base; our products are unbiased, third-party evaluations of current and emerging SUAS technologies

Impact – RAPS directly benefits

Users and manufacturers

FAA by making important contributions toward establishing performance standards and best-practice guidelines

3

Approach

Evaluate performance and utility of mature, DODdeveloped SUAS-sensor combinations using:

– Key capability measures

– One test – ours – applied uniformly to all systems evaluated

– Realistic operational scenarios and environments

– Test reports produced for each system tested

4

Key Test Factors

Operational capabilities

– Example: Does SUAS support routine operations by improving situational awareness?

Operational utility

– Example: Is SUAS easy and efficient to assemble, launch, operate, recover, and pack up?

– Example: Is video output seen effectively at multiple remote terminals?

Technology transition

– Example: Is FAA authorization permitting SUAS operation in the NAS likely?

5

Scope

Test categories

– Scripted operational scenarios

– Operational utility assessments

– Use in National Airspace System

Technical scope

– Daytime testing, < 400 ft, < 25 lb

RAMPS: Robotic Aircraft for

Maritime Public Safety

– New S&T-USCG RDC partnership to test SUAS for maritime applications

New/future capabilities

– Onboard collision avoidance; counter-spoofing; severe storm response

6

Border Security

Rapid response

̶ Improved situational awareness and agent safety

̶ High-value assets in remote, inaccessible, dangerous AORs

Relatively low unit costs could provide:

̶ Many more air assets for target identification and tracking

̶ Eventually, complete aerial coverage of the U.S. border

7

7

RAPS Test Range

Oklahoma Training Center – Unmanned Systems (OTC-US)

Location: Elgin, OK, adjacent to Ft. Sill U.S. Army Post and within Ft. Sill restricted airspace

OTC-US site (red outline)

OTC-US is a test facility of the Oklahoma State

University’s University Multispectral Laboratory “Liberty City” site (urban scenarios)

8

Vendor Participation

• We developed 21 Performance Goals

(see Back-Up) and released an RFI ( Sept.

2012) inviting manufacturer participation: 72 white papers received

• S&T–Manufacturer CRADAs enable testing

̶ No exchange of funds

̶ Vendors provide: SUAS, sensors; pilots, sensor operators, flight support team and equipment

• To date, 15 CRADAs for testing 26 SUAS

DHS S&T is leveraging hundreds of millions of dollars of SUAS technology developed by DOD and the IC, including tens of millions of dollars of industry IR&D investments

9

Test Reports

Reports

– Created by S&T RAPS team for users

– Approved for release by DHS S&T

– Posted and archived online

Websites and access

– Gov’t employees & gov’t-sponsored stakeholders access RAPS Reports via http://www.firstresponder.gov

S&T Communities of Practice site, https://communities.firstresponder.gov

RAPS Community of Practice site

– Access controlled by S&T & RAPS PM

10

Test Reports, cont’d

Test Reports

̶ Content: Complete test results, including scoring summary tables; general

SUAS information; company-proprietary cost and other information

̶ Audience: Restricted to government employees and government-sponsored stakeholders interested in RAPS (potential users)

̶ Access to Test Reports:

• Available upon request to RAPS Program Manager

• Available online at Robotic Aircraft for Public Safety (RAPS) Secure

Community of Practice website

Executive Summaries of Test Reports

̶ Content: Highlights of test results (non-proprietary; company-approved)

̶ Audience: Approved for public release (goal: to reach a wide readership)

̶ Access to Executive Summaries:

• Available upon request to RAPS Program Manager

• Available online at Robotic Aircraft for Public Safety (RAPS)

Community of Practice website

11

Rating Summaries

To facilitate SUAS comparisons, each Report contains Rating Summaries of results in our 54 Performance Measures in 5 Assessment categories: A1. Law Enforcement; A2.

Search and Rescue; A3. Fire Response; A4. Operational Utility; A5. Operation in NAS

Above: Sample Rating summary information

Performance Measure (PM)

Scoring Keys for

Qualitative and

Quantitative Ratings

Unit, Rating (bar-graph), T & O markers Qual., Quant. Rating

12

RAPS Schedule (Cycle 1)

Test

Week

1

2

3

4

5

6

7

8

9

Test

Date

Dec. 10-14,

2012

Jan.14-18,

2013

Mar. 11-15,

2013

Apr. 15-19,

2013

May 13-17,

2013

June 10-14,

2013

June 17-21,

2013

July 15-19,

2013

Aug. 26-30,

2013

Company

Lockheed Martin ADP

AeroVironment

Honeywell

Leptron

(Tactical Electronics)

Aeryon Labs

UAS Dynamics

Lockheed Martin MS2

Mission Technology

Systems, LLC

AeroVironment

Platform(s)

Stalker (Blk 15),

Stalker XE (Blk 10)

Puma AE, Raven B,

Wasp AE (Blk IV)

T-Hawk (Blk II)

Avenger; R.A.P.T.R.

Scout V1, SkyRanger

Skylark

Desert Hawk III,

Desert Hawk-EER, Indago

Buster

Qube, Shrike

√ √

13

RAPS Schedule (Cycle 1)

Test

Week

10

11

12

13

14

N/A

15

16

17

Test

Date

Sept. 9-13,

2013

Oct. 21-25,

2013

Dec. 9-13,

2013

Jan. 13-17,

2014

Jan. 27-31,

2014

April 14-25,

2014

May 12-16,

2014

May 19-23,

2014

June 16-20,

2014

Company

AirRobot

Prioria

Falcon UAS

Applied Research Assoc.

AirCover/Lockheed Martin

CBP (PSI Tactical)

UAV Solutions

Stark Aerospace

Aurora

Platform(s)

AR100B, AR100C, AR200

Maverick, VMAV

Falcon

Nighthawk

QR425

InstantEye

Talon, Allerion, Phoenix30

BirdEye 400, Mini-Panther √

Skate √

14

Lessons Learned

No one platform performs well in all scenarios

Fixed-wing aircraft:

̶ Very good in search and rescue (SAR), fire monitoring

̶ Some fixed wing SUAS need operating areas > 200 ft radius

• Launch and recovery zones

• Deep stall landings affected by winds

Rotary-winged aircraft:

̶ Perform well in crime, accident, and arson scene investigation, and in SWAT

̶ Hover ability is very beneficial

̶ Some systems are relatively quiet, providing stealth, and can “perch”

̶ Up to 50-min endurance was tested/verified – winds are not a limiting factor

(flying in winds up to 30 mph)

̶ In winds, maintain commanded flight profiles better than fixed wing aircraft

15

Lessons Learned, cont’d

Essential capabilities for effective, high-use operations:

̶ Integrated EO and IR sensors on a stabilized, gimbaled platform

• SAR aided by ability to switch between two modes to validate Targets of

Interest (TOI)

• Dual sensors are valuable in urban scenarios where shadows are prevalent

̶ Geo-referenced EO and IR full motion video

• Needed for chain of custody and TOI location accuracy

Collision avoidance:

̶ For some systems, the best way to avoid oncoming traffic may be to initiate immediate landing – but climb and descend speeds may not be sufficient to avoid collision

Other findings:

̶ Quiet systems developed by DOD may need audible augmentation during SAR

̶ The fuel cell SUAS we tested is a significant new capability: > 8 hr endurance

• Note to potential users: It requires > 12 min for warm-up prior to launch

16

Future Outlook

Cycle 1, FY2012-14

• 2012

– Range selection; advocacy

– Define program scope and set key partnerships

– RFI; Test Plan; contracting

• Stand up:

– Processes to work with manufacturers, create and disseminate reports

– Liaison to DHS privacy working group

• Conduct 19 flight test weeks

• Analyze and disseminate results from Cycle 1 testing

Cycle 2, FY2015-16

• New RFI; new Test Plan

• Expanded test scope (goals):

– Fire/HAZMAT/disaster, SAR response

– Specialized SUAS sensors

– Larger, more complex operational scenarios

– Counter-spoofing and antijamming capabilities

– Airworthiness

• Severe storm response pilot

– RAMPS new start: Maritime testing, USCG RDC-led collaboration

– Transition Plan for future funding and management structure

17

Project Office, Web Links

RAPS Project Support Officer:

– Mr. Kevin Spence: (202) 254-2235 kevin.spence@associates.hq.dhs.gov

RAPS and related Web Links:

– http://www.firstresponder.gov

is a public-access DHS S&T website

– Government employees and government-sponsored stakeholders interested in RAPS may request access to the RAPS Test Reports via http://www.firstresponder.gov

, which is the gateway to access S&T’s First Responder Communities of Practice site, https://communities.firstresponder.gov

, which is the gateway to the RAPS Community of

Practice site. Access is controlled by DHS S&T and the RAPS Program Manager.

RAPS Request for information (RFI), released September 24, 2012: https://www.fbo.gov/spg/DHS/OCPO/DHS-OCPO/DHS13-01/listing.html

RAPS Privacy Impact Assessment (PIA), approved Nov. 16, 2012, was the first such document addressing unmanned aircraft ever published – anywhere in the world: http://www.dhs.gov/sites/default/files/publications/privacy/PIAs/privacy_pia_st_ raps_nov2012.pdf

18

SUAS Performance Goals

Common Requirements: Threshold

Lost Link Procedures Rally Point

Airframe Accumulated Flight Time

Sensors

Sensors (EO/IR)

Laser Designation

Training (operator)

Deployment

Recovery

Assembly

Ready to launch (after assembly)

Mean time between lost link

Airworthiness–Operator’s Manual

Airworthiness–Maintenance Manual

Weight (MTO)

> 200 hr (rotary); > 500 hr (fixed)

Electro-optical and infrared

Fixed

None

One week

Bungee/catapult launch

Line/net capture

< 5 min

< 5 min

> 100 hr flight time

Provide written Operator’s Manual

Provide written Maintenance Manual

< 25 pounds

Rotary-winged UAS: Threshold Objective

Endurance 30 min 1 hr

Range

Speed (dash)

Speed (endurance)

Altitude

0.25 mi

10 mph

0 mph

400 ft AGL

1 mi

30 mph

20 mph

1000 ft AGL

Service Ceiling 6,000 ft MSL 10,000 ft MSL

Acoustic signature (400 ft AGL) 70 dBA 40 dBA

Objective

Rally Point, after time return to launch

> 400 hr (rotary); > 1,000 hr (fixed)

Chemical/biological/radiological

Gimbaled

Laser spotter integrated

One day

Hand launched

Deep stall/hover

< 1 min

< 1 min

> 250 hr flight time

Provide written Operator’s Manual

Provide written Maintenance Manual

< 25 pounds

Fixed-winged UAS: Threshold Objective

Endurance 30 min 2 hr

Range

Speed (dash)

Speed (endurance)

Altitude

1 mi

20 mph

15 mph

400 ft AGL

3 mi

40 mph

30 mph

1000 ft AGL

Service Ceiling 6,000 ft MSL 10,000 ft MSL

Acoustic signature (400 ft AGL) 70 dBA 40 dBA

20

RAPS STEERING GROUP

Dr. John Appleby, Chair

Mr. Bob Griffin, Director

Mr. Jonathan Cantor

Ms. Tamara Kessler, Chief (Act.)

Mr. John Priddy, Director

Capt Doug Nash, Chief

Mr. Chris Vaughan

Mr. Jim Williams, Director

Mr. David Morton

DHS S&T HSARPA

DHS S&T First Responder Group

DHS Chief Privacy Officer (Act.)

DHS Office for Civil Rights and Civil Liberties

DHS Customs and Border Protection (CBP)/ Air Operations

DHS U.S. Coast Guard/ Office of Aviation Forces

DHS Federal Emergency Management Admin./ Geospatial Management Office

Federal Aviation Administration (FAA)/ UAS Integration Office

FAA/ UAS Integration Office, Aviation Safety Inspector

Mr. Steve Pansky

Dr. Steve McKeever

Mr. Eric Meyn, Director

FAA/ UAS Integration Office, Senior ATC Analyst

Oklahoma State Univ./ VP for Science &Technol. Transfer; UML/ Executive Director

University Multispectral Laboratories (UML)/ Unmanned Systems Division

Chief Robert Doke

Chief Jon Hansen

LTC Jon Greenhaw

Mr. Mike O’Shea

Cmdr Bob Osborne (ret.)

Oklahoma State Fire Marshall

Director, Oklahoma Council On Firefighter Training (COFT)

Oklahoma National Guard

Department of Justice/ Office of Justice Programs

Los Angeles County Sheriff’s Department

Chief Donald Shinnamon, Sr. (ret.) Public Safety Aviation Consultant

Mr. Andy Lacher MITRE Corporation/ UAS Integration Research Strategist

21

PRIVACY

http://www.gigapixel.com/image/gigapan-canucks-g7.html

22

Download