Path: utzoo!utgpu!news-server.csri.toronto.edu!cs.utexas.edu!sdd.hp.com!zaphod.mps.ohio-state.edu!pacific.mps.ohio-state.edu!linac!att!cbnews!cbnews!military From: pur-ee!luj@gus16.ecn.purdue.edu (Jun Lu) Newsgroups: sci.military Subject: Re: F-117A performance? Message-ID: <1991Feb13.223541.8373@cbnews.att.com> Date: 13 Feb 91 22:35:41 GMT References: <1991Feb5.043703.6484@cbnews.att.com> <1991Feb6.033318.22925@cbnews.att.com> <1991Feb7.021146.4777@cbnews.att.com> Sender: military@cbnews.att.com (William B. Thacker) Organization: Purdue University Engineering Computer Network Lines: 23 Approved: military@att.att.com From: pur-ee!luj@gus16.ecn.purdue.edu (Jun Lu) > >The F-18 is also designed with an inherent pitch instability. This allows > it to pitch up rather quickly, while the computer gives the plane the > illusion of great stability. F-18 drivers often comment on how they love Computer deos not give the illusion. Neither can it provide stability mystically. It is the on board _control system_ that does job -- it generates the control signal using feedback principal, and acutators receving the signals produce control forces to affect the control surfaces(aileron, rudder, ...)of the airplane. This effectively modifies the closed-loop system's dynamics, making it a stable system. For F-18, it uses a digital controller, implemented by a digital computer. which just runs the control algorithms and generates the control signal ... Actuators do the physical job ... -- -- Jun Lu Internet:luj@ecn.purdue.edu -- -- Aeronautics & Astronautics Bitnet: luj%ecn.purdue.edu@purccvm -- -- Purdue University UUCP: pur-ee!luj -- -- W. Lafayette, IN 47907 Phone:317-494-9410 Fax:317-494-0307 --