Open Access. Powered by Scholars. Published by Universities.®

Aeronautical Vehicles Commons™

Open Access. Powered by Scholars. Published by Universities.®

Articles 31 - 36 of 36

Full-Text Articles in Aeronautical Vehicles

Cubesat: Performance Evaluation Of A Deployable Thin Film Solar Array, Michael Forbis, Ian Prager, Matthew Veldhuis Apr 2002

Cubesat: Performance Evaluation Of A Deployable Thin Film Solar Array, Michael Forbis, Ian Prager, Matthew Veldhuis

Robert "Bob" Twiggs STEM Education Collection

A PowerPoint Presentation created by Michael Forbis, Ian Prager, and Matthew Veldhuis titled CubeSat: Performance Evaluation of a Deployable Thin Film Solar Array" from April 23, 2002.


Hypercube Team 1: Space Sciences And Technology Demonstration, Jim Albers, Mike Dowler, Kathy Lee, Gordon Maahs, Steve Sears Apr 2002

Hypercube Team 1: Space Sciences And Technology Demonstration, Jim Albers, Mike Dowler, Kathy Lee, Gordon Maahs, Steve Sears

Robert "Bob" Twiggs STEM Education Collection

A PowerPoint Presentation created by Jim Albers, Mike Dowler, Kathy Lee, Gordon Maahs, and Steve Sears titled "HyperCube Team 1: Space Sciences and Technology Demonstration" from April 23, 2002.


Stanford Microsats, Robert J. Twiggs Apr 2002

Stanford Microsats, Robert J. Twiggs

Robert "Bob" Twiggs STEM Education Collection

A PowerPoint Presentation created by Professor Bob Twiggs titled "Stanford MicroSats" from April 5, 2002.


Suppression Of Pilot-Induced Oscillation (Pio), Donald A. Johnson Mar 2002

Suppression Of Pilot-Induced Oscillation (Pio), Donald A. Johnson

Theses and Dissertations

Closed loop instability caused by excess phase lag induced by actuator rate limiting has been suspected in many pilot-induced oscillations (PIOs) and oscillatory departures from controlled flight. As part of the joint AFIT/TPS program, a longitudinal pilot command notch filter activated by a real-time oscillation verifier (ROVER) algorithm was developed to eliminate the PIO source for any developing, severe PIO. Closed loop computer simulations were conducted to prepare for the flight test. The HAVE ROVER flight test project was flown using the NF-16D Variable Stability In-flight Simulator Test Aircraft (VISTA). A programmable heads-up display (HUD) was used to generate a …


New Technologies For Rapid Space Experiments: Preliminary Design Review, Robert J. Twiggs Feb 2002

New Technologies For Rapid Space Experiments: Preliminary Design Review, Robert J. Twiggs

Robert "Bob" Twiggs STEM Education Collection

A PowerPoint Presentation created by Professor Bob Twiggs titled "New Technologies for Rapid Space Experiments: Preliminary Design Review" from February 25, 2002.


University Space Programs & Collaborative Space Research, Robert J. Twiggs Feb 2002

University Space Programs & Collaborative Space Research, Robert J. Twiggs

Robert "Bob" Twiggs STEM Education Collection

A PowerPoint Presentation created by Professor Bob Twiggs titled "University Space Programs & Collaborative Space Research" from February 8, 2002.