SHAKEEL MOZAFFAR
Pilots at 88 Pl, Ocala, FL
License number
Florida A2581082
Issued Date
Jun 2015
Expiration Date
Jun 2017
Category
Airmen
Type
Authorized Aircraft Instructor
Address
Address
7110 SE 88Th Pl, Ocala, FL 34472
Professional information
Aircraft Attitude Systems
US Patent:
8421649, Apr 16, 2013
Filed:
Feb 21, 2011
Appl. No.:
13/031370
Inventors:
Jerry Lee Marstall - Asheville NC, US
Shakeel Mozaffar - Ocala FL, US
Shakeel Mozaffar - Ocala FL, US
International Classification:
G01C 23/00
US Classification:
340975, 340967, 340974, 701 4, 701 14
Abstract:
Aircraft attitude systems are provided, in which a representative system includes: an instrument face having a bank angle scale, a bank status indicator, a pitch angle scale and a pitch status indicator; the bank angle scale being fixed in position relative to the instrument face and being operative to present increments of bank angle of an aircraft; the bank status indicator being operative to move relative to the bank angle scale such that a current aircraft bank angle is indicated; the pitch angle scale being fixed in a vertical orientation relative to the instrument face and being operative to present increments of pitch angle of an aircraft; the pitch status indicator being operative to move relative to the pitch angle scale such that a current aircraft pitch angle is indicated.
Aircraft Attitude Systems And Related Methods
US Patent:
8290641, Oct 16, 2012
Filed:
Apr 13, 2010
Appl. No.:
12/758903
Inventors:
Jerry Lee Marstall - Asheville NC, US
Shakeel Mozaffar - Ocala FL, US
Shakeel Mozaffar - Ocala FL, US
Assignee:
Pilot Disorientation Prevention Technologies, L.L.C. - Dover DE
International Classification:
G01C 5/00
US Classification:
701 9
Abstract:
Aircraft attitude systems are provided. A representative aircraft attitude system includes: a detection system operative to determine an attitude of an aircraft in which the detection system is mounted; a warning system operative to alert a pilot when the attitude of the aircraft corresponds to at least one predefined attitude parameter from a set of predefined attitude parameters, the predefined attitude parameters including pitch, bank and yaw; and a recovery system operative to provide progressive flight control positioning directives to the pilot for returning the aircraft to a flight attitude within the predefined attitude parameters.