The Sikorsky Cypher UAV

The Cypher, a ducted rotor UAV airplane with a composite shroud structure, fly-by-wire controls, integrated aeronautics, and an aboard mission laptop. This UAV is equipped with a range of payloads, like detector packages, with a weight up to forty lbs. The symmetrical, rounded shroud safely encloses the rotor system, and produces a stealthy signature. The vehicle will operate autonomously per a preplanned mission or below communication system via a data-link  Cypher incorporates a hover capability, 3 hour flight endurance, and its high speed of seventy knots permits flights up to twenty five kilometers.

Flight demonstrations of the Cypher technology demonstrator craft were conducted by the sikorsky craft corporation. Intended for military and civil applications. These demonstrations embrace capabilities like ground and armed service police investigation, communications relay and countermeasures missions, non-defense roles as counter-narcotics, ordnance disposal, forestry, utilities, enforcement and search and rescue.

The Cypher UAV is 6.5 feet in diameter. It combines the potency of a ducted airstream with a homocentric advancing blade idea rotor system. The rotors and also the circular shroud that encloses them can share in providing carrying capacity. Powered by a 50-horsepower category engine, Cypher UAVs are able to cruise at eighty knots, for up to 3 hours, with a ceiling of 8,000 feet. Cypher shares each automatic target detection and fly-by-wire control systems with the Boeing industrialist RAH-66 Comanche chopper being developed for the military.

uav
Cypher UAV
Photo: paper-replika.com

As an autonomous, or “smart” air vehicle, Cypher holds position and navigates employing a differential world Positioning System. The air vehicle is in a position to fly “hands-off,” rather than being flown directly by a ground operator. It additionally showed a capability to land remotely, camera-directed by its aboard tv, on slopes as high as fifteen degrees. Confined space operations showed it kicking off and landing between obstructions even twelve feet apart.

The enclosed rotor idea developed by sikorsky is safer than exposed UAV rotor systems. The Cypher style, with the rotor system within a shroud, minimizes the hazard of exposed high speed rotor blades to ground personnel. The Cypher incorporates composite structures, bearing-less rotors, fly-by-wire flight controls, advanced aeronautics. It works plainly and utilizes a centralized laptop, known as the vehicle mission processor, for execution of flight control laws, vehicle management functions, direction computations, flight payload management and air vehicle communications.

Cypher’s UAV autonomous flight modes are auto take-off and landing, position hover-hold, altitude hold, rate hold, way-point navigation and UAV return-home. Implementation of the return-home mode permits the operator to command the vehicle back to the first launch location – or the other preset location – with simply a push of the button.

The Cypher vehicle is controlled and monitored from an integrated mobile ground station. The whole mission is planned, operated and monitored from one system manager monitor. Vehicle and payload commands, from the system manager, are relayed to the UAV airplane via a digital telemetry transmission. UAV altitude  mission knowledge, surveillance knowledge and payload video are incorporated into one downlink signal that’s transmitted to the management van.

The air vehicle accumulated over four hundred flight hours at Sikorsky’s Development Flight Center in West Palm Beach, Fla., and at various U.S.government demonstrations.

In a demonstration at the Military Operations in Urban Terrain (MOUT) site at Fort Benning, Ga., Cypher flew down streets, landed on a building’s roof and strategically placed varying payloads. For the U.S. Army’s Autonomous Rotorcraft Testbed (ASRT) program, Cypher – with no operator input – searched and tracked man-size targets. For the U.S. Department of Energy, Cypher used magnetometers to go looking and find underground structures and tunnels in Nevada. In Sep 1997, Cypher flew at the Army’s Force Protection equipment Demonstration in Virginia.

Other Cypher demonstrations enclosed flights at Indiana’s test bed for detection of loaded ordinance and also the Army personnel college at Fort McClellan, Ala., wherever the UAV took part during a drug interdiction exercise.

The multi-use Security and surveillance Mission Platform (MSSMP), started in FY’92 because the Air-Mobile Ground Security and closed-circuit television (AMGSSS), was intended to produce a fast deployable, extended-range police investigation capability for a range of operations and missions, including: readying, force protection, plan of action security, support to counter-drug and patrol operations, signal/communications relays, detection and assessment of barriers (i.e., mine fields, tank traps), remote assessment of suspected contaminated areas (i.e., chemical, biological, and nuclear), and even resupply of little quantities of crucial things. The MSSMP system consists of 3 air-mobile remote sensing packages and a base station.

The MSSMP detector packages could operate as transportable complete units, or from air-mobile platforms. the present style of the air-mobile platforms is based on the Sikorsky Cypher enclosed-rotor vertical-take-off-and-landing Unmanned air vehicle. This air-mobile platform carries its detector package from one ground surveillance location to a different, up to ten kilometre from the original station.

A portable mission payload Beta package was developed by a team of SSC engineers and scientists, and a further payload package was integrated onto the Cypher vehicle by Sikorsky and SSC engineers. In May 1996, the system was successfully shown at the military college at ft. McClellan, AL, during a simulated counter-drug operation. The portable detector package mounted on a ground vehicle-of-opportunity and also the Cypher-mounted detector package were both operated at the same time over a similar radio network.

In January 1997, the MSSMP system’s continued role was shown during Military Operation in Urban areas situation at the Dismounted Battlespace Battle Laboratory, Ft. Benning, Georgia. The system showed reconnaissance support with the vehicle flying down town streets, searching through upper- and lower-story windows, providing lookout support prior to advancing troops, and performing observations when landing on the roof of a 2 story building. The vehicle additionally dropped a simulated radio relay on the highest of a building, a miniature intrusion detector in an open field, and carried a customary Army optical device rangefinder/designator as a payload.

The AMGSSS idea grew from NRaD’s expertise with the ground Air Telerobotic System (GATERS) program, initiated in 1986 by the United States Marine Corps. NRaD (then the Naval Ocean Systems Center (NOSC)) was the principle development agent on the system. GATERS consisted of a land-based, Tele-Operated Vehicle (TOV) and the Airborne Remotely Operated Device (AROD). The TOV was developed to perform remote reconnaissance/surveillance with fire and target designation/ranging capabilities. The TOV supported a High-Mobility-Multi-Wheeled-Vehicle (HMMWV) platform while AROD provided mobile intelligence reconnaissance. The TOV used a fiber-optic communications link to produce the required bandwidth in non-line-of-sight operations. The military users did not need to be encumbered with the fiber-optic tethers and preferred that one operator be able to supervise many remote systems.

The AROD was a ducted fan VTOL air vehicle that would easily translate through the air and supply aerial surveillance. The AROD was controlled from a mobile ground control station over a fiber-optic data-link, with a radio link as a back up. AROD had shorter flight endurance and payload capabilities. The AMGSSS idea marries the fast quality and low-data-rate management aspects of VTOL platforms with the long endurance reconnaissance capabilities of the unmanned ground vehicles.

Boeing’s Phantom Ray

         The Phantom Ray, part of Boeing’s Project Reblue, is a demonstrator aircraft which except for a select few engineers and executives was kept a secret, even within the company until May 2009. The stealth unmanned combat air vehicle was conceptualized in 2007 but not in full swing until in June 2008. May 10, 2010 The phantom ray was presented after which the aircraft was scheduled to complete, in 6 months, 10 test flights show casing its ability’s in mock scenarios such as  intelligence, surveillance and reconnaissance; suppression of enemy air defenses; electronic attack; hunter/killer; and autonomous aerial refueling. The Phantom ray made is first flight, after a series of delays, in  April 27, 2011.

UAV Boeing
Photo: Boeing
            The Phantom Ray has a length of 36ft (11m), a 50ft (15m) wingspan, its maximum take off weight is 36,500ib (16,556kg), with a maximum speed of Mach 0.85 and a cruising speed of 614mph (Mach 0.8), and has a range of 1,500mi (2,414km). Boeing first development for the Defense Advanced Research Projects Agency (DARPA), the U.S. Air Force, and the U.S. Navy Joint-Unmanned Combat Air System (J-UCAS) programs was the X-45C prototype that the phantom Ray was modeled after. Its current status is Under development however Boeing suspects that  that the Phantom Ray will be the first of a new prototype aircraft series.

Northrop Grumman’s X-47B

The X-47B first flew in 2011 at Edwards Air Force Base in California, it began as a project for DARPA’s J-UCAS program but soon adopted the goal of becoming a carrier based unmanned air craft and is now part of the United States Navy Unmanned Combat Air System Demonstration program. The Northrop Grumman X-47B is similar to the Boeing X-45, the original concept design being the X-47A Pegasus that first flew in 2003.
The aircraft is 38.2 ft in length and has a wingspan of 62.1 ft extended/30.9 ft folded. Its height is 10.4 ft with a maximum takeoff weight of 44,567 lb (empty weight of 14,000 lb). In 2000 the Navy gave contracts of $2 million to both Boeing and Northrop Grumman for a 15-month concept-exploration, with a specific goal in mind. The concept had to take into account the corrosive saltwater environment, launch and recovery on deck, integration with command and control systems, and operation in an aircraft carrier’s high-electromagnetic-interference environment, as well as the ability to perform reconnaissance missions.
Photo courtesy of en.wikipedia.org

The Navy chose Northrop Grumman’s X-47B in 2006 after the J-UCAS program was cut and the navy began its own UAV program. The X-47B has an unrefueled range of over 2,000 miles (3,200 km), and an endurance of more than six hours. In November of 2011 the Navy announced that aerial refueling equipment would be added to one of the prototypes in 2014. After performing so consistently during the preliminary test flights, The X-47B will be used to demonstrate carrier launches and recoveries, as well as unmanned in-flight refueling with a probe and drogue.

May 2012, at Patuxent River, AV-1 began high-intensity electromagnetic interference testing to ascertain its compatibility with planned electronic warfare systems. The project was started out funded under a US$635.8-million contract awarded by the Navy in 2007. However, by January 2012, the X-47B’s total program cost had grown to an estimated $813 million. 

Predator B vs Altair unmanned airplanes

Predator B Vs. Altair

PREDATOR B

ALTAIR

Military Multi-Mission ISR

High-Altitude Scientific Research

Wingspan:

66 ft (20.1168m)

Fuselage:

36 ft (10.9728m)

Weight:

10,000 lb (4536 kg)

Altitude:

50,000 ft

Endurance:

30+ hr

Payload:

Internal – 800 lb (363 kg)

External – 3,000 lb (1361 kg)

Powerplant:

Honeywell TPE 331-10T

Air Speed:

Over 220 kn

Customer:

U.S. Air Force

Wingspan:

86 ft (26.2128m)

Fuselage:

36 ft (10.9728m)

Weight:

7,000 lb (3175 kg)

Altitude:

52,000 ft

Endurance:

30+ hr

Payload:

Internal – 660 lb (300 kg)

External – 3,000 lb (1361 kg)

Powerplant:

Honeywell TPE 331-10T

Air Speed:

TBA

Customer:

NASA

Predator B 3d model

The Predator B, developed in 2000, had its first flight in February 2001. The airplane is powered by a turboprop engine; the Predator B series was built to be a long-endurance, high-altitude unmanned aircraft for multiple uses with appeal to a variety of customers. Surveillance, targeting, and weapons delivery are just a few of the possible applications of this craft as well as scientific research and other civilian applications. The Predator B has the ability to maintain multiple missions simultaneously thanks to its large internal and external 

payload capacity.

       
      


 

       The Altair was designed to be a high altitude version of the Predator B. It was specifically designed as an unmanned craft for both scientific and commercial research missions. The air craft meets the requirements of endurance, reliability and increased payload capacity. The craft was built in partnership with NASA, the Altair has an 86 ft wingspan, can fly up to 52,000 ft.; It can remain airborne over 30 hours. It is the first remotely piloted aircraft that will meet aviation authority requirements for unmanned flights in National Air Space. Altair is currently being integrated with an automated collision avoidance system and an air traffic control voice relay to increase responsiveness and communication for flights in National Airspace.

source: uavinfo.org

Aviation and Airplane Performance

        There are quite a bit of factors that can affect aircraft performance. If you don’t keep in mind these factors you may find yourself in a dangerous situation where you will receive a violation from the FAA or even worse, dead. Aircraft manufacturers provide this information in the form of charts. These are generally located in the Performance section of the POH. Performance charts are usually shown as a table or graph. To get the most accurate result you must use all the chart procedures and guidelines.


        Two factors affecting airplanes are the weight of the airplane and wind. The groundspeed and time en route can change due to the wind direction and speed. Since we know that performance decreases with altitude we also know that decreases in air density due to temperature, pressure, or humidity will also cause a decrease in performance. Humidity is usually disregarded due to the maximum affect only being a 7% decrease.


        Another large reason to determine performance is landing and taking off distance. This can make the difference between hitting an obstacle or rolling of a runway. The runway gradient is the amount of change in the slope of a runway over its length. A gradient of 2% means the slope changes 2ft for every 100ft of runway. A positive gradient may be favorable for landing as it will require less room to slow down, but it also makes it unfavorable to take off due to increased force required to push the airplane up the slope. Takeoff and landing charts for each specific airplane help tremendously with calculating these numbers.

aircraft takeoff chart
An example of a takeoff  distance chart from a CESSNA POH book

        The best angle of climb airspeed is normally used for obstacle clearance immediately after takeoff. Due to a higher pitch attitude your forward visibility is also decreased. Usually you use the best rate of climb after clearing all obstructions. This will give you the highest climb rate. Before an airplane can gain altitude it must have a reserve of thrust. The service ceiling of an aircraft refers to the altitude where an aircraft is only able to climb 100 feet per minute. This is commonly referred to as absolute ceiling since it represents the practical ceiling for the aircraft.