DANIEL DEXTER VILLANI
Pilots at Corona Ave, Long Beach, CA

License number
California A2699568
Issued Date
Oct 2016
Expiration Date
Oct 2018
Category
Airmen
Type
Authorized Aircraft Instructor
Address
Address
305 Corona Ave, Long Beach, CA 90803

Professional information

Daniel Villani Photo 1

Owner At Dv Astronautics Consulting

Position:
Owner at DV Astronautics Consulting
Location:
Greater Los Angeles Area
Industry:
Aviation & Aerospace
Work:
DV Astronautics Consulting - Long Beach, CA since Mar 2013 - Owner Semi Retired Engineer, budding SF author - Home Jul 2012 - Mar 2013 - Retired SpaceX - Hawthorne, CA May 2008 - Jul 2012 - Lead Mission Operations Engineer Boeing Satellite Systems 1975 - 2008 - Associate Technical Fellow
Education:
Princeton University 1983
Ph. D., Aerospace Engineering
California Institute of Technology 1965 - 1969
B. S., Physics
Escambia County High School 1963 - 1965
Skills:
Spacecraft, Space Systems, Systems Engineering, Aerospace, Satellite, System Design, Engineering Management, Orbital Mechanics, Aerospace Engineering, Propulsion, Requirements Management, Requirements Analysis, Integration, System Testing, Testing, Avionics, System Architecture, Satellite Communications, Engineering
Languages:
Conversational Spanish


Daniel Villani Photo 2

Combined Roll-Yaw Spacecraft Steering Method For Low Earth Orbit Target Trajectory Compensation

US Patent:
6288670, Sep 11, 2001
Filed:
Dec 23, 1999
Appl. No.:
9/470701
Inventors:
Daniel D. Villani - Long Beach CA
Harold A. Rosen - Santa Monica CA
Assignee:
Hughes Electronics Corporation - El Segundo CA
International Classification:
H04B 7185
US Classification:
342354
Abstract:
For an antenna on a satellite in an inclined orbit about the Earth, cross-track motion resulting from the rotation of the Earth can be reduced in antenna coordinates by yawing and/or rolling the antenna (preferably by yawing and/or rolling the entire satellite, for example, by using a reaction wheel system) by an appropriate angle, which varies throughout the orbit.


Daniel Villani Photo 3

Alignment System For Encoders

US Patent:
4772872, Sep 20, 1988
Filed:
Dec 12, 1986
Appl. No.:
6/940885
Inventors:
Daniel D. Villani - Long Beach CA
Assignee:
Hughes Aircraft Company - Los Angeles CA
International Classification:
H03M 126
US Classification:
341 9
Abstract:
An improved encoder alignment system is disclosed which provides an indication of the extent of misalignment and a measure of the rate at which the misalignment may be changing. The invention is adapted for use with a conventional encoder which provides a digital coarse word having at least significant bit and a digital fine word having a least significant bit and a most significant bit. The invention generates the exclusive or of the least significant bit of the coarse digital signal and the least significant bit of the fine digital signal to provide a first signal. The invention then generates the exclusive or of the first signal and the complement of the most significant bit of the fine digital signal to provide an output signal which represents the misalignment of the encoder.


Daniel Villani Photo 4

Magnetic Systems And Methods For Realizing Spacecraft Maneuvers

US Patent:
6089510, Jul 18, 2000
Filed:
Jul 30, 1997
Appl. No.:
8/903109
Inventors:
Daniel D. Villani - Long Beach CA
Peter B. Landecker - Manhattan Beach CA
Assignee:
Hughes Electronics Corporation - El Segundo CA
International Classification:
B64G 132
US Classification:
244166
Abstract:
Spacecraft maneuvers (e. g. , orbit transferring, stationkeeping and attitude controlling) of a first spacecraft are realized with conventional force and torque generators (e. g. , thrusters and momentum wheels). Spacecraft maneuvers of a second spacecraft are realized through magnetic interaction between the first and second spacecraft. In particular, a magnetic moment vector m. sub. 1 of a magnetic system of the first spacecraft and a magnetic moment vector m. sub. 2 of a magnetic system of the second spacecraft are adjusted to apply selected force vectors and torque vectors to the first and second spacecraft.