F-35 Joint Strike Fighter

Joint Strike Fighter (JSF) is the name for a family of fighter aircraft#multirole fighters being built in three versions:

• F-35A Lightning II: Conventional takeoff and landing, not carrier-capable, specifically for United States Air Force requirements. Will replace A-10 Warthog and F-16 Fighting Falcon; complements F-22 Raptor
• F-35B Lightning II: Short takeoff and vertical landing, meeting the environmental requirements of shipboard use, but not catapulted. To be used by the Italian Navy, U.K. Royal Air Force and Royal Navy, United States Marine Corps; will replace assorted versions of the Harrier aircraft.
• F-35C Lightning II: Conventional takeoff and landing, carrier-capable and catapult-launched, for United States Navy requirements. Will replace F-18 Hornet but not necessarily F-18 Super Hornet

JSF, in U.S. doctrine, is the "low" end of the fighter mix, the "high" end being the F-22 Raptor. Both the F-22 and F-35 are considered fifth generation jet fighters.

Avionics

Avionics are among the features that make the F-35 fifth-generation. They interconnect in a modular, upgradable manner. Much of the avionics will be common, with the most extensive fit in the Air Force model. Interconnection of avionics is not limited to MIL-STD-1553B, but als o includes IEEE 1394 Firewire and Fibre Channel. There are triple-redundant computers and Firewire buses in the Vehicle Management Computers of the Vehicle Management System for flight control, which act as the master for each bus. The bus cables are cross-connected so a cable failure can be circumvented.

While 1553 handles some legacy functions, most processing is over 1394b

Given the importance of software, if the U.S. desires export control, it may be more a matter of what programming is included in a model, rather than what hardware devices are included

As with the F-22, much of the system is built around an AESA radar. A diference, however, is that EOTS is mounted in parallel with it.

Computing and networking

The two interface modules, one per rack, link the CNI processors with the F-35 integrated core processor. Where signals leave the aircraft, they are encrypted. The aircraft uses a hybrid of MIL-STD-1553 bus for controlling existing weapons and systems, but COTS high-speed interfaces for such things as video over Fibre Channel.

Many of the components are reprogrammable before or during flight. Software defined radio, for example, is the standard.

System	Baseline	Direction
Processors	7 Power PC, 5 signal/data processing; 2 interface
Bus	MIL-STD-1553	Fibre channel for high-bandwidth sensors
UHF/VHF radio	SDR for testing 6/2006
radar altimeter
intercom
identification-friend-or-foe
CNI suite	9/2006

Flight controls

Components residing on the 1394b network serve the following systems, from a combination of computing and input/output devices supporting 10 remote units: Vehicle Systems Processing, VMC and RIO (10 remote input/output units);

• Flight Control Systems: rudders, flaperons, horizontal tails, ailerons, air data probes, inertial electronics, and crash-survivable memory units
• Utilities and Subsystems such as weapons bay door drives, power system controllers, brake controllers, and thermal management system controllers;
• Propulsion Systems such as Full Authority Digital Electronic Control (FADEC) over the main engine
• Mission Systems including display management, lighting controller, communications/navigation/identification, and GPS;
• Flight data acquisition and recording

Sensors

There are five basic sensor systems:

• The AESA phased-array radar,
• The electro-optical targeting system (EOTS) with forward-looking infrared (FLIR) and infrared search and track (IRST) system,
• The electronic warfare suite, developed by BAE Systems,
• The electro-optical distributed aperture system (DAS), and
• The communication, navigation and identification (CNI) suite, providing identification friend or foe (IFF) and offboard data delivered via a high-speed data link.

Perhaps the most guarded capability on the F-35 is its automatic target recognition. Lockheed Martin would only say that the aircraft will be continuously processing sensor detections regardless of the orientation (air or ground track). "Some tracks can be easily and rapidly resolved and categorized, while others will require some extensive processing to resolve ambiguities," says a Lockheed official. For automatic target identification, he adds, the F-35 aircrew "will be able to choose target types during the preflight mission planning process."

Radar

As does the F-22, the F-35 will have a AESA phased-array radar, but a different one, the Northrop Grumman AN/APG-81 from the F-22's AN/APG-77. The two systems have significant commonality, but the F-35 probably has more ground targeting capability. The F-22 has more air combat and electronic warfare ability in its radar.

It is likely the two systems will converge, as the AN/APG-63 V(4) will eventually serve both the F-15 Eagle and F-15E Strike Eagle.

EOTS

When physically looking at the F-35's avionics, the EOTS, at first, might seem to be missing. After all, other aircraft either put it into a pod attached to a pylon, or has a turret.

On closer examination, the EOTS is there, operating through a sapphire window in the F-35 nose, just below the AESA radar antenna. Coaxial EOTS and radar help cross-cueing between EOTS and radar, as opposed to the situation where the EOTS is shifted to a wing-mounted pod.

DA

One unique feature of the F-35 is the distributed aperture system, a set of six infrared cameras on the top, side, rear, etc., of the aircraft, so the pilot will have no blind spots; every possible view can be displayed on the "glass cockpit' screen.