Return-Path: Received: from olympus.net ([198.133.237.6]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-64832U3500L350S0V35) with ESMTP id com for ; Thu, 10 Aug 2000 20:35:46 -0400 Received: from pt19476.olympus.net ([207.149.194.76] helo=station4) by olympus.net with smtp (Exim 3.12 #1) id 13N2tp-00074I-00 for lancair.list@olsusa.com; Thu, 10 Aug 2000 17:42:14 -0700 Message-ID: <00ca01c0032c$fba1c060$0464a8c0@station4> From: "John Barrett" <2thman@olympus.net> To: "Lancair Mail List" Subject: Re: Computed AOA Date: Thu, 10 Aug 2000 17:09:07 -0700 X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> >Does the SFS unit actually know how many G's you're pulling? If so, the >accuracy you credit it with should be good enough for stall warning, even if >it assumes a gross weight. If not, it's no better than an airspeed indicator. Yes the SFS does measure G forces and uses them to compute AOA. I had a discussion with Nate Calvin of SFS a few days ago regarding programming requirement to allow pilot input of initial weight and computer adjustment during the progress of the flight to account for fuel burn. He told me that they had considered this aspect and thought it would be necessary when designing the system, but when it came to practicality and actual flight testing in GA aircraft, the difference was shown to be inconsequential. Therefore weight is programmed as a constant. Regards, John Barrett - LIVP CARBINGE- "The World Hinges on Us" 360 385 1000 http://www.olympus.net/personal/2thman/carbinge1.htm >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>