Hood River, OR - The first flight test of the T2 gimbal was successfully conducted on April 24, 2008. The test was executed using a prototype gimbal mounted on the strut of an Air Commander Darter under wind conditions gusting to 31 knots. The primary goals of the test were to exercise the new drive system and to assess the stabilization performance of the gimbal. The results were outstanding; the stabilization and object tracking performance allowed repeatable hands-off autonomous tracking of moving vehicles for over one minute even at a 2 degree field of view during significant aircraft motion. The progress shown with this sustained tracking capability was due to new software developments by Cloud Cap Technology’s partner company Solution Engineering Inc.
Infrared imaging using the new Flir 640 Photon with a 35mm f/1.4 lens was also successful; the production T2 will feature the 640 Photon with a 62mm f/1.25, delivering 14 degree FOV imagery. T2 qualification testing continues with successful environmental testing from -50°C to +80°C and shock, vibration, and additional flight testing planned in the near future.
Need help defining your Piccolo autopilot system? The Piccolo Configuration Wizard is the answer! Building a full avionics solution, complete with an autopilot, ground station, and developer’s kit, can be very complex given the number of configuration options.
The Piccolo Configuration Wizard is a new web based system configuration tool designed to help customers define and tailor Piccolo system elements to best meet the needs of their project. The wizard conveniently matches radios, ground stations, and advanced features, which simplifies the system building process.
At the end of the wizard you can print a complete configuration list, and if desired, have the list sent to Cloud Cap to get a formal quotation via e-mail. Take a tour of the Piccolo Configuration Wizard and let us know what you think!
Hood River, OR - Cloud Cap Technology has been very pleased with the initial testing of the newest Tier II gimbal, the T2 over the last few weeks. Senior Engineering Technician, Dan Underwood stated, “It’s been very successful so far. We wanted to test the current levels created by wind loading on the motors. We are very pleased with the results.” Lead Engineer Rob Gilchrist added, “Wind load generated large power draw was our biggest concern on this product, and we’re happy to see it perform so well during these initial tests.”
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The T2 is the newest gimbal in the TASE family of gimbals, building on inertial stabilization technology developed in the TASE and TASE Duo products. T2 has been in development for the past six months and is set to debut at this year’s AUVSI tradeshow in June.
It has been nine years since founders Ross Hoag and Bill Vaglienti, veterans of the Aerosonde UAV development program, set out with a goal of developing an avionics system for small unmanned aerial vehicles (UAVs). They knew that the avionics system had to be small, low cost, and low power. This concept evolved for the first two years of the company’s existence until a core set of autopilot requirements were worked out. In the fall of 2001 all of these requirements came together to produce the first Piccolo avionics system and ground station.
Since then the Piccolo family of products has grown to include an expanded line of autopilots, payloads, and sensors.
From its humble beginnings of two innovative engineers, the Cloud Cap team has grown to more than twenty engineers, technicians, and support personnel with over 70 years of combined experience in the UAV field.
Cloud Cap Technology looks forward to many more years of serving our customers by continuing to provide powerful low cost integrated solutions to the UAV market.
December 19, 2007, Hood River, OR - Cloud Cap Technology, Inc is pleased to announce attendance at the following 2008 tradeshows. Our aim is to present live demos on site for each of our product lines. Come by to see the Piccolo Autopilots, TASE Gimbals, and Crista IMUs and find out how our products can benefit your integration project. We are considering a number of other exhibit opportunities - please check this space for further tradeshow announcements in 08.
AUVSI's Unmanned Systems North America 2008
June 10 –12, 2008. San Diego, CA
Booth 1139
Map - top row, center of map.
Farnborough International Airshow
July 14-20, 2008. Farnborough, UK
AUVSI UAV Pavillion, Hall 1, Booth B16
Floor plan – top, left of center.
Airborne Law Enforcement Annual Conference and Exposition
July 16-19th, 2008. Houston TX
Booth 502
Floor plan - bottom, center.
To schedule an appointment or for more info, contact:
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November 26, 2007, Hood River, OR - Cloud Cap Technology, Inc. is pleased to announce a new partnership with Guided Systems Technologies to provide Piccolo autopilot solutions for helicopter and other rotary wing unmanned vehicles. Guided Systems Technologies, leveraging more than 18 years of experience in guidance and control, offers advanced flight control technology that has been proven on a wide variety of unmanned rotary wing vehicles, including single main rotor and coaxial helicopters, tilt rotors, ducted fans, tail sitters and airplanes that can hover on the propeller.
Piccolo autopilot products are now capable of full-envelope automated helicopter flight operations, including take-off and landing, precision hover, automated path following and autopilot assisted manual steering modes. Additionally, Guided Systems will provide comprehensive customer support from initial project requirements definition through qualification flight testing.
Dr. Eric Corban, Guided System’s Founder and CTO says, “The helicopter and rotary wing UAV market will benefit greatly from affordable access to a complete helicopter control solution proven over a number of flight test programs that is made relatively easy to integrate through the combination of advanced technology, integrated hardware, quality documentation, and support that is tailored to the needs of the rotorcraft community.”
The Cloud Cap Technology family of Piccolo autopilots have become the standard for fixed wing UAV integrators. All of the Piccolo options provide a complete, off-the-shelf avionics system solution including the core autopilot, flight sensors, navigation, wireless communication, and payload interfaces, all in a small, highly-integrated, and inexpensive package. Over 1,500 autopilots have been delivered to date. The Piccolo autopilot is currently in service on a wide range of vehicles including the ACR Silver Fox, the Raytheon Cobra and the NAVAIR Tiger Shark UAV. Detailed information and system documentation for the Piccolo autopilots can be found at www.cloudcaptech.com.
For additional information contact:
| Young Kim Guided Systems Technologies (770) 898-9100 x895 |
Mark Zanmiller Cloud Cap Technology (541) 387-2120 x 27 |
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November 7-8, 2007 Tucson AZ – Today Advanced Ceramics Research (ACR) and Cloud Cap Technology (CCT) demonstrated moving capture precision recovery using a Piccolo II equipped Silver Fox UAV with the latest 2.X autopilot software. During the two days of testing the team was ten for ten on autonomous recovery attempts, which included a variety of moving net scenarios. This was the first flight test of the moving capture algorithms and demonstrated the capability required for autonomous shipboard recovery. Shipboard testing will follow early next year. The flight test marks the culmination of a one-year development effort led by Bill Vaglienti, CCT’s co-founder and CTO, and builds upon the initial release of the 2.X branch of Piccolo autopilot code which supported fixed position precision recovery. With the addition of moving capture precision recovery the Piccolo System now supports options for autonomous rolling takeoff, catapult, balloon and tube launching; as well as wheeled, belly, shipboard or land based precision net recovery.
Background
Advanced Ceramics Research
(ACR) is a leading developer of small UAS systems
for the Department of Defense. Their Silver Fox UAV is currently deployed
in Iraq in support of Operation Iraqi Freedom. ACR provided the Silver Fox
UAV, ground infrastructure, flight operations crew, as well as designed and
implemented the moving net system used during the testing. ACR is one of
CCT most valued customers; historically they have been a driver as well as
an early adopter of new Piccolo technology. A special thanks goes out to
the ACR team who were instrumental in making this flight test possible.
Cloud Cap Technology (CCT) is the world leader in end user programmable UAV autopilots systems, payloads, and sensors. The Piccolo family of autopilots, Piccolo II, Piccolo Plus, and Piccolo LT, provide unparalleled performance, reliability, and flexibility at an affordable price. The Piccolo system offers a complete solution including modeling and simulation tools, documentation and support as well as a new full-featured user interface called Piccolo Command Center (PCC).
For additional information contact:
| Mark Zanmiller Cloud Cap Technology (541) 387-2120 x 27 |
Matt Pobloske Advanced Ceramics Research (520)-573-6300 |
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Piccolo equipped Silver Fox UAV Flies in the Philippines for the 31st MEU. October 19, 2007 - Fort Magsaysay, Philippines - Providing a forward set of eyes from above, the 31st Marine Expeditionary Unit, III Marine Expeditionary Force, launched the Silver Fox unmanned aerial vehicle for the first time to conduct an operational evaluation here, Oct. 19, during Amphibious Landing Exercise '08. For more information, see the full article in the UAV News.
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Cloud Cap Technologies TASE Gimbal used in QinetiQ's Zephyr UAVSeptember 10, 2007, White Sands NM - A TASE gimbal, produced by Cloud Cap Technology Inc. was successfully used as the imaging payload in QinetiQ’s Zephyr High Altitude Long Endurance (HALE) Unmanned Aerial Vehicle (UAV).
At the US Military's White Sands Missile Range in New Mexico the Zephyr achieved a 54 hour endurance flight, unofficially breaking the world record of 30 hours and 24 minutes.
The Zephyr is an ultra-lightweight carbon-fiber aircraft with a wingspan of up to 18 meters but weighing just 30 kg. By day it flies on solar power generated by silicon arrays no thicker than sheets of paper that cover the aircraft's wings. By night it is powered by batteries that are recharged during the day using solar power. During the trials the same aircraft was flown twice while carrying the TASE gimbal as a surveillance payload – first for 54 hours to a maximum altitude of 58,355 feet, and then for 33 hours 43 minutes to a maximum altitude of 52,247 feet. Potential applications for Zephyr include earth observation and communications relay in support of a range of defense, security and civil requirements. Additional details of the Zephyr accomplishments can be seen in the QinetiQ news release.
The Cloud Cap Technology TASE gimbal provided features key to the QinetiQ efforts. It is a robust, small and very light weight stabilized payload. The TASE gimbal electrical and mechanical interfaces and inherent flexibility allowed QinetiQ to achieve HALE performance with an inexpensive < 1Kg gimbal.
For additional information about Cloud Cap Technology and the TASE family of stabilized camera gimbals, please contact at 541-387-2120 x 27.
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Cloud
Cap Technology Releases 2.x Branch Software August 6 , 2007 - Hood River, OR - Cloud Cap Technology Inc. announces the release of software version 2.0.4 for the Piccolo family of autopilots. Software branch 2.x has been in development for more than a year and integrates the 6 years of development experience from the 1.x software branch. Important features of version 2.0.4 includes new system capabilities, control law implementations, integration support, and a significant new user interface, the Piccolo Command Center. As with previous Piccolo software, an open communication specification, SDK, and licensable source provide users with flexibility of use and options for customization. As with previous Piccolo software versions, the new autopilot software is provided free for to Piccolo customers to download. Source code licensing and advanced feature licenses are provided on a fee basis.
The new system capabilities provide precision autonomous takeoff and landing, including rolling or catapult takeoff, and wheeled, net, and or belly recovery with full support for flare, brakes, and on the ground steering. Balloon and tube launch support are also provided . A new full GPS/INS navigation solution with fixed wing aided AHRS backup in case of GPS failure adds to system robustness and performance. Optional integration with high-end dual frequency RTK DGPS receivers provide centimeter-level position accuracy for applications where precision recovery is required.
New advanced control laws have been implemented for higher fidelity control of fixed wing platforms. A universal controller API is added, making it easier to change the control laws for new platforms including helicopters, blimps, boats, etc. As such, 2.x supports the long anticipated Piccolo helicopter solution which will be led by Cloud Cap’s rotary wing partner, Guided Systems Technologies.
Customer modeling and integration is further assisted with new advanced vortex lattice simulator tools which ease the estimation of aircraft parameters. I/O configuration is made even more flexible, allowing customer configuration of up to 16 outputs for servo or discrete surface and payload management. All of these items support reduced time for customer integration of a new platform.
The 2.x release also includes the new Piccolo Command Center interface software. This completely new Piccolo interface, developed by Solution Engineering Inc. addresses requirements from current users and provides a powerful solution which significantly improves the flexibility and feature set provided. Key features include enhanced flight planning support, map display improvements with multi-aircraft displays and 2D/3D terrain aware mapping, a new intuitive Primary Flight Display and graphical EFIS along with the ability to change airspeed, altitude, and heading commands from EFIS display. Design allows user customizable dockable windows so data can be configured per user requirements.
For more information, contact:
| Bill Vaglienti Cloud Cap Technology, Chief Technology Officer (541) 387-2120 x 22 |
Ross Hoag Cloud Cap Technology, President (541) 387-2120 x 23 |
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July 23, 2007,
Hood River, OR - Today Cloud Cap Technology officially
kicked off an eighteen-month program to develop a small, low cost, stabilized
pan tilt and zoom camera gimbal system called TASE LT. This smaller
version of the popular TASE is being designed specifically for the NAVAIR
expendable Sonabuoy Launched UAV (SLUAV) program but will have wider application,
especially in the emerging small electric UAV market. Additionally, and
most importantly from a cost and size perspective, the proposed Cloud Cap
Technology solution will combine the autopilot and gimbal functionality
into a single common autopilot/gimbal electro-mechanical package resulting
in a dramatic reduction in the overall size, complexity, and cost compared
to any competitive solutions. Given our long history and expertise in autopilot
technology, Cloud Cap Technology is uniquely qualified to provide this
additional level of functionality in the gimbal package. This novel approach
offers the optimal solution given the size and cost constraints of expendable
systems of this class.
Cloud Cap Technology will be teaming with both Solution Engineering (SEI) and Currawong Engineering Pty Ltd on this program. Solution Engineering, another Hood River company, will be developing advanced video processing capabilities (including target tracking and electronic stabilization) which will be embedded onboard the TASE LT. Currawong Engineering, an Australian company located in Hobart, Tasmania will be working on the mechanical design and prototyping.
The program is being funded under a NAVAIR Phase II SBIR program focused on developing payload solutions for the NAVAIR Coyote and Voyeur UAVs. The base program includes a twelve-month development effort followed by a six-month evaluation and demonstration period. An option, if exercised, will be targeted toward integration of the TASE LT on to other existing small-electric UAVs. The addition of a stabilized camera gimbal and advanced video processing, which until recently has not been available to vehicles of this class, will dramatically expand their Intelligence, Surveillance, and Reconnaissance (ISR) potential.
For more information contact:
Ross Hoag at (541) 387-2120 x 23
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Raytheon's Cobra Unmanned Aircraft System Makes a Series of Firsts in North Dakota.

Photo by Ben Trapnell, University of North Dakota
July 11, 2007 -TUCSON, Ariz., PRNewswire -- A Raytheon Company Cobra Unmanned Aircraft System (UAS) conducted the first official unmanned aircraft flight in North Dakota June 25.
The Cobra flew approved flight profiles through military restricted airspace over Camp Grafton South, a National Guard training facility 45 miles south of Devil's Lake, N.D.
In addition to being the first unmanned aircraft to fly in North Dakota airspace, these were also the Cobras' first flights away from their home station in Tucson, Ariz.
During the three-day deployment to the site, the Cobras completed nine flights and executed completely autonomous takeoffs, landings and in-flight navigation along preplanned routes.
The flights were part of Raytheon's collaboration with the University of North Dakota, John D. Odegard School of Aerospace Sciences, the University of North Dakota School of Engineering and Mines and the North Dakota National Guard.
In one of the planned missions from the Camp Grafton South airfield, a Cobra UAS carried the PrecisionAg digital imaging payload developed by the University of North Dakota Unmanned Aircraft Engineering team. The PrecisionAg payload is designed to take digital images of crops and rangeland for monitoring vegetation health for North Dakota agribusiness applications.
"With its ability to conduct completely autonomous flight profiles and its FAA experimental airworthiness certification, Cobra is positioned to be the preferred unmanned aircraft system for the science, research and engineering communities," said Don Newman, Raytheon director of Unmanned Systems. "Cobra can stay aloft for more than three hours with a 25-pound payload, providing researchers with an affordable, stable platform for an array of sophisticated electronic equipment and sensors."
Cobra is a low-cost, highly reliable unmanned aircraft designed to support Raytheon's development, integration and test of unmanned systems technologies. The aircraft has a wingspan of 10 feet and is 9-feet long.
The Cobra UAS was designed by Raytheon to support the development, test and demonstration of sensor systems; networked command, control and communications systems; and unmanned aircraft system architectural concepts. The Cobra UAS integrates advanced systems and capabilities from several Raytheon businesses, including Tucson-based Missile Systems; Intelligence and Information Systems, based in Garland, Texas; Space and Airborne Systems in El Segundo, Calif.; and McKinney, Texas-based Network Centric Systems.
Raytheon Company, with 2006 sales of $20.3 billion, is a technology leader specializing in defense, homeland security and other government markets throughout the world. With a history of innovation spanning 85 years, Raytheon provides state-of-the-art electronics, mission systems integration and other capabilities in the areas of sensing; effects; and command, control, communications and intelligence systems, as well as a broad range of mission support services. With headquarters in Waltham, Mass., Raytheon employs 73,000 people worldwide.
Contact:
Everett Tackett, APR
520.794.9494
Virginia Tech’s team pulled out a win and pulled in $9000 at the AUVSI –sponsored Student UAS competition in late June.
The competition, at Naval Air Station Patuxent River’s Webster Field, in St. Inigoes, MD., called for the teams to take off or land autonomously, fly several waypoints while staying within pre-set boundaries and detect targets on the ground, wooden words that spelled out “Go NAVAIR.” Although this year’s target was similar to last year’s “Go Navy,” competition director Joe Brannan says no team was able to do it. Adding to the challenge were brisk winds blowing across Webster Field.
Virginia Tech completed the competition using the Piccolo LT Autopilot from Cloud Cap Technology. Overall, three of the top seven teams used Piccolo products in their aircraft (although the Embry-Riddle team ultimately removed their Piccolo for fear of crashing it in the high winds).”

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Cloud
Cap Technology Piccolo Guides T-15 High Altitude Return Vehicle (HARV)
- Demonstrates autonomous recovery from 63,684 feet.June 29, 2007 - McGregor Range, Fort Bliss, NM - the AFRL/AFSC HARV was balloon launched from Wilde Benton air strip (4,068') on McGregor Range in southern New Mexico. The goal of the test was to demonstrate the capability to cost effectively deploy and autonomously recover a high altitude payload from 65,000 feet. The vehicle used was a modified electric T-15 developed by Arcturus UAV. The T-15 was equipped with a Cloud Cap Technology Piccolo II autopilot, General Dynamic's payload, video system, and both UHF and Satellite communications. The vehicle's full-up weight at launch was 42 pounds including 10 pounds of payload (half its 20 pounds capability).
It took 52 minutes to ascend, with balloon float occurring at 63,684
feet. Two minutes later the HARV was released and began the initial freefall
portion of the decent. Autonomous pullout was accomplished thirteen seconds
later at 61,500 feet. During the pullout the HARV achieved a maximum
velocity of 200 KTS (True Air Speed) and pulled 2.75 g's. The HARV then began tracking back to base, arriving nine minutes later at 49,344 feet, where it began a long gliding descent. Fifty-six minutes later at 5,000 feet (932 feet AGL) the system initiated a landing flight plan at which point the engine was enabled and the HARV
began an autonomous approach and landing. Total sortie time was just over two hours with about seventy minutes of autonomous flight time after the release.
This test was part of a phased effort co-sponsored by AFSPC and AFRL. The goal was to prove the operational feasibility of the T-15 UAV as a platform for launch and recovery of payloads at 65,000 feet and above.
Also present at the test were representatives from the Army Space & Missile Defense Command, Army Battle Lab, Colorado Springs, Navy Research Lab, and Arizona National Guard, Detachment 2.
For more information, contact:
| Doc Aguilar AFRL/VS (505) 846-5545 |
Len Hirschi Arcturus UAV (707) 206-9372 |
Ross Hoag Cloud Cap Technology (541) 387-2120 x 23 |
Piccolo II autopilot is part of third unmanned aircraft system to achieve FAA experimental airworthiness certification.
Raytheon Receives FAA Experimental Airworthiness
Certificate for Cobra Unmanned Aircraft System.
TUCSON, Ariz., Nov. 2, 2006 - Raytheon Company's (NYSE: RTN) Cobra Unmanned Aircraft System (UAS) is the third unmanned aircraft and the first of its size to receive an Experimental Airworthiness Certificate from the Federal Aviation Administration (FAA).
Cobra is a low-cost, highly reliable UAS designed to support Raytheon's development, integration and test of unmanned systems technologies. The aircraft has a wingspan of 10 feet and is 9-feet long. The certification is the first given to a small UAS and permits Cobra flight operations in a specified section of the National Airspace in Southeastern Arizona. It also authorizes Raytheon to conduct research and development, crew training and market surveys using the Cobra UAS.
The Cobra UAS integrates advanced systems and capabilities from several Raytheon businesses, including Tucson-based Missile Systems; Intelligence and Information Systems (IIS), based in Garland, Texas; Space and Airborne Systems in El Segundo, Calif.; and McKinney, Texas-based Network Centric Systems. The Cobra test bed will be used to support the development, test and demonstration of sensor systems; networked command, control and communications systems; and UAS architectural concepts.
"The Cobra UAS will significantly decrease costs and compress schedules for bringing new UAS technologies to market," said Ken Pederson, vice president of Missile Systems' Advanced Programs. "Our customers will benefit from our ability to support both internal Raytheon development efforts and their programs with Cobra, without increasing the pressure on tactical systems and valuable range resources."
Raytheon worked closely with the FAA to receive the Experimental Aircraft Certification, providing Cobra UAS design, manufacturing, maintenance, safety, operations and training documentation for its review and approval. The final step in the certification process was a demonstration of Cobra UAS ground operations conducted under the observation of FAA teams from Washington and Phoenix.
Raytheon Company, with 2005 sales of $21.9 billion, is an industry leader in defense and government electronics, space, information technology, technical services, and business and special mission aircraft. With headquarters in Waltham, Mass., Raytheon employs 80,000 people worldwide.
Note:
The Cobra UAS is composed of the aircraft and ground elements. The ground
element consists of two control systems -- the Cloud Cap Technology Piccolo
Ground Control Station and the Raytheon IIS next-generation Multi-Vehicle
Control System. The MVCS uses the NATO Standardization Agreement (STANAG)
4586 interface to communicate with the Cobra aircraft. The dual control
system configuration provides for maximum flexibility and safety during
testing.
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The Cloud Cap Technology Piccolo LT comes alive!
May 11, 2006 - Hood River, OR - Today the final pieces arrived that allowed us to assemble the first complete Piccolo LT autopilot. Piccolo LT is a compete autopilot system – it includes the inertial and air data sensors, processing, communications, GPS and flight termination, all fully integrated in a shielded enclosure. Piccolo LT is similar in concept to its big brothers Piccolo Plus and Piccolo II, both in performance and level of integration, but it’s much smaller, only ¾ of an inch thick. Its small size and packaging makes it the ideal solution for the latest generation of small UAV’s.

Figure 1 - Piccolo LT (complete)
We believe Piccolo LT is the worlds smallest “complete” autopilot system. The overall solution weighs in at 109 grams (3.84 oz), which includes everything required – inertial and air data sensors, GPS, flight termination, data link, plumbing, and a shielded enclosure. While others make claims of small size and low cost, once you add in the other required components and do the final electro-mechanical integration you typically end up with a solution that has a much larger footprint, weighs more than anticipated, is electro-mechanically kludged together, and costs more than an integrated solutions. Piccolo LT is a leap forward from any existing technology in its size range, both in performance and level of integration, and will be backed by the same industry leading engineering, production, and application support as the rest of the Piccolo family.
At this point we have fully functional LT hardware and flight software, the production tooling is complete, and the automated test and calibration software is operational (the first LT board has passed inertial and temperature calibration). Our next step is to complete environmental qualification then proceed to flight-test. We expect to introduce the Piccolo LT as well as our new stabilized camera gimbal at AUVSI in late August.

Figure 2 - Piccolo LT (board only)
Related information:
For further information contact:
Mark Zanmiller
Cloud Cap Technology
2621 Wasco Street
PO Box 1500
Hood River OR, 97031
1 541 387-2120 x 27
www.cloudcaptech.com
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May 4th, 2006 - Hamilton, Australia
Aerosonde Mark 4 obtains 38 hour 48 minute endurance mark.
Here's a quick "unofficial" report on the endurance flight:
We flew two aircraft this week in Hamilton, western Victoria to see just how long a Mark 4 Aerosonde could fly. The conditions weren't ideal with several cold fronts passing through the region. These fronts brought cool weather, rain and strong southwesterly winds. Winds at times were higher than the ideal cruise speed of the aircraft and so, coupled with a wet airframe and turbulent conditions, reduced our maximum endurance from our target of 40 hours. The reduced endurance meant that we had to land Aircraft 156 early to ensure we weren't forced to land at night.
Aerosonde 156 (Piccolo II 1053) launched on Tuesday May 2 at 0739 UTC and landed on Wednesday May 3 at 0742 for a total of 24 hours and 3 minutes. It landed with around 2.2 kg of usable fuel.
Aerosonde 157 (Piccolo II 1032) launched on Tuesday May 2 at 0637 UTC and landed on Wednesday May 3 at 2119 for a total of 38 hours and 48 minutes. It was Aerosonde 157's (and probably the Piccolo's) maiden flight and is the first Aerosonde flight to witness 2 sunrises.
Both aircraft landed unscathed apart from a broken static tube. Fuel consumption during the mission ranged from 207grams/hr down to 122 grams/hr.
Many thanks to all the crew at Aerosonde and Cloud Cap Technology that made this achievement possible. We're looking forward to breaking our record again soon.
Maurice Gonella - Special Operations Manager, Aerosonde Pty Ltd
The endurance achievement outlined above is particularly gratifying for Bill and I; it feels like we’ve come full circle with Piccolo flying in the Aerosonde. A 38-hour maiden flight, first flight on both the airframe and avionics, is impressive and shows the maturity level of the individual systems. Most people don’t appreciate what an achievement this is or how much time, effort and expertise are involved to get to this level of “off the shelf” performance.
The Cloud Cap Technology team has a long history with the Aerosonde program; many of us started our UAV careers working on the original Aerosonde back in 1994. It should be noted that the Aerosonde was the target vehicle which drove the original Piccolo design back in 1999 – we envisioned Aerosonde would be one of our first customers. We see this demonstration as the beginning of long and fruitful relationship, two companies with leading edge technology teaming to create world-class solutions.
Congratulations to our long time friends at Aerosonde!
Ross and Bill
Portable Ground Station Kit Now Available
January 2006 - Hood River, OR - The Portable Ground Station Kit (900-90015-00) provides a Piccolo Ground Station incorporated into a 18 x 14 x 7 inch case that makes it portable and more suitable for field operations than the desk top unit. All interface connections and control switches are provided on the outside of the case and associated cables and antennas fit within the case. Provisions are included for mounting an alternate link radio and Iridium satellite communications modem. For details, see the Piccolo System Kit and Ground Station page.
Portable Ground Station Kit (900-90015-00)
For past news items, see our News Archive...