Clifford S Brust5195 Bigger Rd, Dayton, OH 45440

Clifford Brust Phones & Addresses

5195 Bigger Rd, Dayton, OH 45440 (937) 654-1210

3864 Highmont St, Dayton, OH 45432

Beavercreek, OH

North Myrtle Beach, SC

Vandalia, OH

Montgomery, OH

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Defense & Space

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Senior Software Engineer At Sierra Nevada Corporation

Location:
Dayton, Ohio Area
Industry:
Defense & Space
Experience:
Sierra Nevada Corporation (Privately Held; Defense & Space industry): Senior Software Engineer,  (November 2009-Present) Technical project leadership, real-time software design, development, and integration of advanced airborne electronic systems.Defense Research Associ...

Publications & IP owners

Us Patents

System And Method For Producing Flight Pathway

US Patent:
7505835, Mar 17, 2009
Filed:
Jul 3, 2002
Appl. No.:
10/189814
Inventors:
Clifford S. Brust - Beaver Creek OH, US
Gary Evans - Troy OH, US
Assignee:
L-3 Communications Avionics Systems, Inc. - Grand Rapids MI
International Classification:
G01C 23/00
US Classification:
701 3, 701 4, 701 18, 701120, 701122, 701300, 340945, 340947, 340963
Abstract:
A system and method for displaying a three-dimensional image of airspace includes a series of translucent, horizontal “pavers” that lie like stepping stones marking the selected flight path. In addition, the display includes a series of vertical rectangles—called “wickets”—which bracket the selected flight path. One or more of the wickets may include a graphical representation of the direction of the aircraft should be flying through the wicket. The system accommodates changes in course by generating a new flight path when instructed to do so. The new flight path is created in a way that assures continuous guidance for the pilot and sufficient time for the pilot to adjust to the new course. The display can include a compass rose which indicates the aircraft's present heading and direction of flight. The compass rose is generated from data representing a traditional two-dimensional view of a compass rose that is rotated using a graphics processor to show a three dimensional view of the compass rose in a plane that appears nearly horizontal in the three dimensional airspace image.

System And Method For Synthetic Vision Terrain Display

US Patent:
2003002, Jan 30, 2003
Filed:
Jul 3, 2002
Appl. No.:
10/189790
Inventors:
Clifford Brust - Beaver Creek OH, US
International Classification:
G06K009/36
G06K009/32
US Classification:
382/294000, 382/284000
Abstract:
A synthetic rendering of the terrain within a selected field of view is created from raw terrain elevation data, and the resolution of the rendering is proportioned to the altitude above ground level (altitude AGL) of the aircraft. All the data points are subdivided into tiles. Only data from tiles within a prescribed field of view are considered for processing; all others are ignored. Within the selected tiles, only some of the terrain elevation data points are passed to the graphics processor for rendering. At maximum resolution, when the aircraft is on the ground or at a low altitude, there are relatively fewer tiles within the field of view and the fraction of the data points from each tile within the field of view passed for rendering is relatively large. As the aircraft's altitude AGL level increases, the field of view also increases in area increasing the number of tiles within the field of view. However, the number of data points forwarded for rendering by the graphics processor is kept approximately constant by selecting progressively fewer and fewer terrain elevation data points from each tile for rendering as altitude AGL increases. Only the data points that lie within tiles inside a prescribed field of view are forwarded to the graphics processor for rendering. Once the tiles have been selected, the terrain elevation data points are grouped in groups of a size that depends on altitude AGL, with more terrain data points in the grouped as attitude increases. Preferably the groups are triangle strips. Only the highest elevation from each group is passed to the graphics processor for rendering.

Aircraft Avionic System Having A Pilot User Interface With Context Dependent Input Devices

US Patent:
2008018, Jul 31, 2008
Filed:
Dec 3, 2007
Appl. No.:
11/949492
Inventors:
Blake R. Getson - Columbus OH, US
Clifford S. Brust - Beaver Creek OH, US
Assignee:
L-3 COMMUNICATIONS AVIONICS SYSTEMS, INC. - Grand Rapids MI
International Classification:
G06F 3/048
US Classification:
715810, 715860
Abstract:
An avionics system having a pilot user interface, and method of interfacing with a pilot, includes providing a display screen and a video processor driving the display screen. A plurality of context dependent input devices is provided. Operation of at least one of the input devices may cause the processor to display a rotary selection list on the display screen. The rotary selection list includes multiple potential selections, each capable of effecting a change in the avionic system when highlighted. At least one of the input devices may be made up of at least one rotary knob. The processor displays a context dependent label for the rotary knob.

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