Abstract: Acquisition of a waveform such as a continuous-phase modulation (CPM) waveform is described. In one embodiment of the invention, the invention is directed to a method and apparatus for acquiring a waveform as defined by MIL-STD-188-181B including the preamble of such a waveform at a performance level defined by the standard. The present invention provides solutions to at least four primary issues presented in acquiring a CPM waveform such as the MIL-STD-188-181B compliant waveform. These primary problems include searching for the preamble, determination of the symbol rate, determination of an initial carrier frequency error (Doppler), determination of an initial carrier phase, and determination of the start-of-message to establish an absolute time marker within the waveform.

Abstract: In-flight entertainment systems provide entertainment for passengers on commercial airline flights. Presently, usually on longer flights, video entertainment is commonly available on in-flight passenger entertainment systems. In-flight entertainment systems can display video on a variety of display monitors ranging from a conventional CRT display to a more modern Liquid Crystal Display (LCD). Generally most displays are connected to the aircraft electronic system via a ARINC 722 connector. The ARINC 722 connector commonly provides an electrical interface between the aircraft and the video system, whether the video system is a CRT or LCD type monitor. With the increasing use of LCD monitors there is a greater need for the ability of the display monitor to be able to report its status. The need for status reporting is increased because the LCD monitors are often greater in number than the prior art CRT monitors and because malfunctions are less obvious.

Abstract: A method and apparatus for managing communication resources between nodes of a network is disclosed. The network utilizes both dynamic and static assignment of communication time slots. The invention includes a plurality of dynamic nodes wherein communication is accomplished as a result of a node's dynamic assignment to itself of specific time slots from a time multiplex structure. At least one static node is also included in the network. The static node does not participate in the dynamic assignment protocol. Instead, a time slot in said time multiplex structure is pre-assigned for communication with the static node. A dynamic node can serve as a surrogate for a static node, relaying communications between the dynamic and static portions of the network.

Abstract: A system and method for enhancing the integrity of an avionics system which uses a pair dissimilar general purpose microprocessors, each running a virtual machine, compiled for its respective processor, from a common original source file; the virtual machines running on a subset of the instructions for each microprocessor and thereby avoiding conditions known or likely to result in defects; the virtual machines running a single or identical avionics program and then voting the results of this simultaneous redundant execution to arrive at an enhanced assurance level; providing written claims to the FAA that an enhanced assurance level is achieved.

Abstract: An aircraft formation/refueling guidance system guides a follower aircraft relative to a leader aircraft. A datalink provides a position hold and a bias command from the leader aircraft to the follower aircraft. An optical tracker onboard the follower aircraft takes an image of the leader aircraft when receiving the hold command, tracks the leader aircraft using the image, and provides optical tracker movement outputs. A resolver resolves the optical tracker movement outputs to provide resolver control signals. A vernier control receives the bias command to change a position of the follower aircraft by biasing the resolver control signals with a bias signal. A sum circuit connected to the resolver and to the vernier control receives the resolver control signals and the bias signal to provide a sum circuit output signal. An autopilot and autothrottle receives the sum circuit output signal and the position hold command to control the follower aircraft.

Abstract: A protocol disclosed for managing an adaptive broadcast channel in a network having nodes communicating via scheduled time slots on a time multiplex basis. The protocol is suitable for use with a dynamic assignment protocol such as USAP. The protocol permits the use of transmitter based broadcasts and receiver directed broadcasts during the same frame. Further, embodiments for implementing explicit and implicit reservation schemes are disclosed. Further still, a technique for increasing efficiency through implementation of an optimized receiver directed broadcast schedule is disclosed.

Abstract: A weather radar display system is disclosed. The weather radar display system comprises a weather radar antenna, processing electronics, coupled to the weather radar antenna, enhancing weather radar returns based on a reflectivity model which differentiates lower level activity from higher level activity when the weather activity is detected from weather systems at long range and the reflectivity using short range thresholds would display only higher level activity. A weather radar display displays multiple colors representative of the different levels of weather activity based on the enhanced returns.

Abstract: A system and method for enhancing the integrity of a system which uses a high performance, low assurance, general purpose microprocessor to execute an avionics software application and uses a high assurance, low performance microprocessor to monitor the output of the general purpose microprocessor, without the need for comparison of outputs from parallel processors executing functionally equivalent versions of the avionics software application. The monitoring microprocessor is used to analyze state transitions of the first microprocessor and to analyze the computed values output by said general purpose microprocessor, against predetermined limitations based upon aircraft limitations.

Abstract: A statechart includes a state having two or more parallel states. The two or more parallel states are ordered to ensure determinism for the system. The statecharts can be modified Harel statecharts. The statecharts can be utilized to generate avionics software.

Abstract: An aircraft weather radar system is disclosed. The system comprises a radar antenna, aircraft sensors, and a database. The system also comprises a processing device receiving information from the radar antenna and from the aircraft sensors and able to retrieve information from the database. Further, the system comprises a cockpit display coupled to the processing device. The processing device is programmed to estimate storm system characteristics based on the received information from the aircraft sensors and the database and to display the storm system characteristics on a vertical weather profile display using a graphical representation.

Abstract: A method of communicating an uncertainty of a location of an object near an aircraft is disclosed. According to the method, a plurality of signals are received from positioning sources. Each of the positioning sources provide information regarding the location of the object. A positional uncertainty of the object is obtained for each of the plurality of signals. Each positional uncertainty is related to an accuracy of the signal to which the respective positional uncertainty relates. The obtained positional uncertainties are combined to derive a combined positional uncertainty of the object having first and second mutually orthogonal directional components. The combined positional uncertainty is expressed as a geometric shape. On a display associated with the aircraft upon which the aircraft and the object are graphically represented, the geometric shape is superimposed on the graphical representation of the object, to thereby apprise a viewer of the positional uncertainty of the object.

Abstract: The invention is an apparatus for lengthening the path of a light beam. The apparatus includes an at least partially enclosed chamber having a first opening and a second opening. A first reflective surface is disposed within the chamber and is obliquely oriented with respect to an incoming path of the beam. The beam reflects off of the first reflective surface after the beam enters the chamber through the first opening. Second and third reflective surfaces are disposed within the chamber and are generally parallel to the incoming path of the beam. The beam is reflected a plurality of times between the second and third reflective surfaces after the beam is reflected by the first reflective surface. A fourth reflective surface is disposed within the chamber and is obliquely oriented with respect to the incoming path of the beam. The fourth reflective surface directs the beam through the second opening after the beam has been reflected a plurality of times between the second and third reflective surfaces.

Abstract: An aircraft FMS/guidance system which provides for automated and immediate calculation of a preferred flight path and full heading, pitch-and-roll guidance along that path for paths of random origins, such as during late-occurring missed approaches and circling-to-land maneuvers.

Abstract: Disclosed are a low pass filter, and a direct conversion receiver (DCR) implementing the same, which filter and second signal channels with improved phase and gain match, allowing use of the filter and DCR in wideband environments. A first M-pole filter channel, comprised of a first plurality of 2-pole active filter stages, filters the first signal channel. A second M-pole filter channel, comprised of a second plurality of 2-pole active filter stages, filters the second signal channel. One of the second plurality of 2-pole filter stages includes two variable components. The values of the variable components of the second M-pole filter channel are adjusted to match the gain and phase of the first and second filter channels.

Abstract: An airborne radar system is disclosed. The airborne radar system comprises a radar antenna, radar circuitry coupled to the radar antenna, and a runway database comprising runway location information. The airborne radar system also comprises a processing device retrieving from the runway database, runway location information for a runway being approached by an aircraft, based on the location of the aircraft, and directing a radar beam defined by a polygon which represents the runway and which is derived from the runway information, the processing device determining whether there are any obstacles on the runway.

Abstract: Deriving inertial-aided deviations for autoland systems during GPS signal interruptions involving an inertial reference system and a GPS landing system can include converting position coordinates of an aircraft from the inertial reference system to runway, lateral, and vertical coordinates. After this conversion, the method calibrates runway distance and lateral distance based on the converted position coordinates from the inertial reference system using runway distance and lateral distance from the GPS landing system with a third-order calibration filter when the aircraft is below a first height above terrain and calibrates vertical distance based on the converted position coordinates from the inertial reference system using vertical distance from the GPS landing system with a second-order calibration filter when the aircraft is below the first height above terrain.

Abstract: An optical coupler is designed to be utilized with multiple light sources. The optical coupler can include a reflecting mirror, a plurality of coupling rods, and an integrating rod. The reflecting mirror receives light from the light sources and reflects light to the coupling rods. The coupling rods provide a path for the light to the integrating rod.

Abstract: The disclosure is directed to a full color liquid crystal display system providing compatibility with Class A night vision imaging goggles. One embodiment of the invention is directed to a color liquid crystal display (LCD) having dual modes of operation. The color LCD display includes a normal mode light source, a liquid crystal display stack positioned so as to receive light from the normal mode light source, and a night vision imaging system (NVIS) mode light source. The NVIS mode light source includes a NVIS mode white light source, a NVIS mode red light source, a NVIS filter receiving light from both the NVIS mode white light source and the NVIS mode red light source, and a waveguide receiving light from the NVIS filter for reflection to the LCD stack.

Abstract: A system employs null angle measurements developed in response to the detection of radiation, such as jamming, along with the positions at which the null angles are measured, to determine the location of the radiation source through reverse triangulation.

Abstract: An apparatus and method for automatically displaying to a flight crew member a list of electronic charts appropriate for a set flight plan or alternatively displaying the appropriate chart in response to information input into an FMS.