Pilot Training Manual
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Ff 89/6 Copy
$3 vol libre • free flight 6/89 Dec - Jan POTPOURRI SAC was informed by Sport Canada on the 10th of July that we are not eligible for funding for 1989-90 and until further notice. Thus we are now totally on our own. The average yearly grant from 1979 to 1988 in 1989 dollars was $14,000, or $16 per person. Perhaps it’s a good thing as planning in an atmosphere of doubt is not conducive to good health and efficient use of funds. The cutback was not unexpected and steps were taken early on to ease the effects of this loss of revenue. Imaginative planning in our small store and a good response from our members through the use of the “Soaring Stuff” inserts resulted in in- creased sales. We will also receive higher than projected invest- ment income essentially due to careful cash management and short-term interest rates, which have remained higher for longer than generally expected. In addition, a small gain in projected receipts from an unexpected increase in membership – now at 1423 – which is the first time since 1982 that we have passed 1400. Total expenditures should come in well below budget projection, primarily as a result of scaling back meetings and travel expenditures. On balance it seems fair to say that a combination of some tight fistedness on the expenditure side and a bit of luck on the revenue side will leave SAC in a financially stronger position than was expected at the beginning of the season, despite the cutting off of govern- ment funding. -
FEDERAL REGISTER VOLUME 30 • Liulvibeil 249
FEDERAL REGISTER VOLUME 30 • liulviBEil 249 Tuesday, December 28, 1965 • Washington, D.C. Pages 16099-16180 Agencies in this issue— Agricultural Research Service Agricultural Stabilization and Conservation Service Atomic Energy Commission Civil Aeronautics Board Commodity Credit Corporation Consumer and Marketing Service Federal Aviation Agency Federal Home Loan Bank Board Federal Housing Administration Federal Maritime Commission Federal Power Commission Federal Trade Commission Food and Drug Administration General Services Administration Interstate Commerce Commission Land Management Bureau Maritime Administration Public Health Service Reclamation Bureau Detailed list of Contents appears inside. Volume 7 8 UNITED STATES STATUTES AT LARGE [88th Cong., 2d Sess.l Contains laws and concurrent resolu merical listing of bills enacted into tions enacted by the Congress during public and private law, and a guide 1964, the twenty-fourth amendment to the legislative history of bills en to the Constitution, and Presidential acted into public law. proclamations. Included is a nu- Price: $8.75 Published by Office of the Federal Register, National Archives and Records Service, General Services Administration Order from Superintendent of Documents, U.S. Government Printing Office, Washington, D.C., 20402 ¿f' Published, daily, Tuesday through Saturday (no publication on Sundays, Mondays, or on the day after an official Federal holiday), by the Office of the Federal Register, National FERERAL*REGISTER Archives and Records Service, General Services Administration (mail address National Area Code 202 V , »3 4 Phone 963-3261 Archives Building, Washington, D.C. 20408), pursuant to the authority contained in the Federal Register Act, approved July 26, 1935 (49 Stat. 500, as amended; 44 U.S.C., ch. -
Nonlinear Control of an Aerobatic RC Airplane
Nonlinear Control of an Aerobatic RC Airplane MASSA CHUSETTS INSTITUTE by 0F TECHNOLOGY Joshua John Bialkowski J UN 2 3 2010 B.S., Georgia Institute of Technology (2007) LIBRARIES Submitted to the Department of Aeronautics and Astronautics in partial fulfillment of the requirements for the degree of Master of Science in Aeronautics and Astronautics ARCHIVES at the MASSACHUSETTS INSTITUTE OF TECHNOLOGY May 2010 @ Massachusetts Institute of Technology 2010. All rights reserved. Author .......... .~. .....-.--...--.-.- D ar o % autics and Astronautics May 21, 2010 Certified by..... Prof Emilio Frazzoli Associate Professor of Aeronautics and Astronautics Thesis Supervisor / / IA Accepted by............. / Eytan H. Modiano Associate Professor of Aeronautics and Astronautics Chair, Committee on Graduate Students Nonlinear Control of an Aerobatic RC Airplane by Joshua John Bialkowski Submitted to the Department of Aeronautics and Astronautics on May 21, 2010, in partial fulfillment of the requirements for the degree of Master of Science in Aeronautics and Astronautics Abstract An automatic flight controller based on the ideas of backstepping is applied to an aerobatic RC airplane. The controller asymptotically tracks a time-parameterized position reference, and depends on an orientation look-up rule to detemine the vehicle orientation from a desired acceleration. A coordinated-flight look-up rule compatible with the controller provides a nominal level of capability for traditional flight trajec- tories. A generalized coordinated look-up rule compatible with the controller provides more advanced capability, including stability for high angle of attack and hovering maneuvers, at the expense of an additional requirement from the reference trajectory. Basic simulation results are used to verify the controller, and a simulation software framework is described which will enable more extensive simulation and provide a platform for the final controller implementation. -
Small Lightweight Aircraft Navigation in the Presence of Wind Cornel-Alexandru Brezoescu
Small lightweight aircraft navigation in the presence of wind Cornel-Alexandru Brezoescu To cite this version: Cornel-Alexandru Brezoescu. Small lightweight aircraft navigation in the presence of wind. Other. Université de Technologie de Compiègne, 2013. English. NNT : 2013COMP2105. tel-01060415 HAL Id: tel-01060415 https://tel.archives-ouvertes.fr/tel-01060415 Submitted on 3 Sep 2014 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. Par Cornel-Alexandru BREZOESCU Navigation d’un avion miniature de surveillance aérienne en présence de vent Thèse présentée pour l’obtention du grade de Docteur de l’UTC Soutenue le 28 octobre 2013 Spécialité : Laboratoire HEUDIASYC D2105 Navigation d'un avion miniature de surveillance a´erienneen pr´esencede vent Student: BREZOESCU Cornel Alexandru PHD advisors : LOZANO Rogelio CASTILLO Pedro i ii Contents 1 Introduction 1 1.1 Motivation and objectives . .1 1.2 Challenges . .2 1.3 Approach . .3 1.4 Thesis outline . .4 2 Modeling for control 5 2.1 Basic principles of flight . .5 2.1.1 The forces of flight . .6 2.1.2 Parts of an airplane . .7 2.1.3 Misleading lift theories . 10 2.1.4 Lift generated by airflow deflection . -
Circular Administration
Advisory US.Depanment 01 Tronsporlolion Federal Aviation Circular Administration Subject: A HAZARD IN AEROBATICS: Date: 2/28/84 At No: 91-61 EFFECTS OF G-FORCES ON PILOTS Initiated by: AFO- 800 ; Change: AAM-500; AAC-100 1. PURPOSE. Because aerobatic flying subjects pilots to gravitational effects (G's) that can impair their ability to safely operate the aircraft, pilots who engage in aerobatics, or those who would take up such activity, should understand G's and some of their physiological effects. This circular provides background information on G's, their effect on the human body, and their role in safe flying. Suggestions are offered for avoiding problems caused by accelerations encountered in aerobatic maneuvers. 2. BACKGROUND. Aerobatic flying demands the best of both aircraft and pilot. The aircraft must be highly maneuverable, yet tolerant of G-loads. The pilot must possess skill and physiological stamina. He or she must be daring, yet mindful of the aircraft's limitations as well as his or her own. Federal Aviation Administration (FAA) Advisory Circular No. 91-48, "Acrobatics-Precision Flying with a Purpose," dated June 29, 1977, discusses some of the airworthiness and operational aspects of aerobatics, but does not consider biomedical factors. The most important of these biomedical factors is the pilot's response to accelerations (or G-loading). The major physiological effects of G-loaaing vary from reduced vision to loss of consciousness. The pilot who understands these effects will be better able to cope with them so that he or she can continue the sport of aerobatic flying. J. -
Stearman Aerobatics
( SFA'OUIFI" OCIOBEF1990 3 AEROBATICS U.S.NAVY Fep ntedlbm: U.S.NAVY PRIMARY FLIGHT TFAINING MANUAL 1 Juy, I945 NAVALAIF TRAINING COMMAND CHIEFOF NAVALAIB PRIMAFYIFAINING o sFA 'OUrFrr'. @TOAEB1990 5 AEROBATICS Import it Regsrdl6 oI sherhd o! not . part.llar manelver lsdecrib€d in th€ lollowlngp!s.i you aE to prc. Youare now !e.dy lor rhar shse in yrlr tEinlnsas a Nav.l dc. only thosemaneuveB d€m6nst6i.d .nd p@scdbedby Aviarlor rowad {hlch you have been lookins loMad wlrh you LndrucrorIn rh2 oda preserr€dby ih€ syllabus keenanricLp,rion, p€rhars nor unmix€dwih 5omeI€€tinqs ot AII .ercb.ric d|l be comDl.r..l !r lad 2,0lr0 f€€r missrvlns.Uk€ manybclore you, 9ou are piobably wondelhg sherhff or nor you can \ak€ i1" ai dre same6me |rboilng Tl ! L nor h.nated .ldtud€ trt .cr!.I .ldtude uider rhedelusionrhanh?maitolasood pilor b hcsktllh aeob.hca $e aE,e'. ol .ou6e. is rhai you qtn be .bl. to "rake ",bu|h? querion$ltbe lnethsornoryouon "h-ue I Yourel€ry b€ll lr sh@ld b. lan.ned snugly.bur mr b Ll" T@ rony c.d?a helore ylo hde (fie ro Ei.t in C r.se, rsh& d ro inrerl€e s h yor les @€m€nis. Ah. simplybea u.e rheyrs'e tanied aky" birthdr entolnenr ol ch4* rh€ shouldq h.66 aerob.rt and r d6n€ ro bercm€ aerbaric expds Tiey 2 Be €@ nor akn in l@kjns lor dhq airEft in your nesleded rh€ prc.kion ert iirrodlc€d i. -
National Transportation Safety Board Aviation Accident Final Report
National Transportation Safety Board Aviation Accident Final Report Location: RANCHO MURIETA, CA Accident Number: LAX88FA015 Date & Time: 10/15/1987, 1528 PDT Registration: N121FJ Aircraft: DASSAULT-BREGUET DA 10 Aircraft Damage: Destroyed Defining Event: Injuries: 3 Fatal Flight Conducted Under: Part 91: General Aviation - Positioning Analysis THE ACFT FLEW TO THE ARPT FOR A SALES DEMO FLT. THE CREW BOARDED THE ACFT AND TAXIED OUT FOR DEP. WITNESSES, INCLUDING TWO PLTS WITH AEROBATIC EXP, WATCHED THE ACFT DEP, MAKE A LEFT TRAFFIC PATTERN AND DO A LOW FLY-BY DOWN THE RWY. AT THE DEP END OF THE RWY, THE ACFT PITCHED UP INTO A STEEP CLIMB. AT 600 FT AGL, THE ACFT ENTERED A LEFT AILERON ROLL, WHICH THE WITNESSES SAID WAS 'SMOOTH, COORDINATED AND WITH THE NOSE ON THE POINT.' AT THE INVERTED POINT OF THE ROLL, THE ROLL CHANGED FROM AN AILERON TO A BARREL ROLL. ONE PILOT WITNESS SAID THAT IT APPEARED THE 'CREW LOST IT AT THE TOP' AND THAT THE CREW 'HELD THE BACK PRESSURE TOO LONG AT THE TOP.' AT THE 270 DEG POINT OF THE ROLL, THE ACFT WAS SEEN TO 'FALL OUT' OR 'DISH OUT' OF THE ROLL; IT RECOVERED TO WINGS LEVEL FLT AT ABOUT 100 FT AGL IN A VERY NOSE HIGH ATTITUDE SETTLING INTO THE GROUND WITH A HIGH VERTICAL DESCENT RATE. NO PREIMPACT ENG OR CONTROL SYSTEM MALFUNCTIONS WERE FOUND. Probable Cause and Findings The National Transportation Safety Board determines the probable cause(s) of this accident to be: IN FLIGHT LOSS OF CONTROL BY THE PILOT FLYING WHILE PERFORMING AN INTENTIONAL LOW LEVEL AEROBATIC MANEUVER. -
Sportsman Sequence but Sequence
SPORT MARCH 2011 OFFICIALFICIAL MAGAZINEMA NENE ofof thet INTERNATIONALN TION AEROBATIC CLUB • First Japanese How to Fly the Contest SPORTSMAN •Cheap Acro SEQUENCE Drive one. 2011 Ford Mustang All Legend, No Compromise The Privilege of Partnership The legendary 5.0L V8 returns to the Mustang GT, delivering 412 HP EAA members are eligible for special pricing on Ford Motor Company and 26 MPG. The 3.7L V6 boasts 305 HP and 31 MPG – new standards vehicles through Ford’s Partner Recognition Program. To learn more in the class! on this exclusive opportunity for EAA members to save on a new Ford vehicle, please visit www.eaa.org/ford. State-of-the-art technology includes: Twin-Independent Variable Cam Timing (Ti-VCT), SYNC in-car connectivity, and AdvanceTrac electronic stability control. VEHICLE PURCHASE PLAN OFFICIAL MAGAZINE of the INTERNATIONAL AEROBATIC CLUB Vol. 40 No.3 March 2011 A PUBLICATION OF THE INTERNATIONAL AEROBATIC CLUB CONTENTS “Somebody said, “Well, they met a black bear when they were making the corner markers. Maybe it’s true. ” Yuichi Tagaki FEATURES 06 Flying the 2011 Sportsman Known John Morrisey 18 Full Circle Dave Watson 22 Cheap Acro Will Tyron 28 Japan’s First Contest Cutting acro out of the jungle Yuichi Takagi COLUMNS 03 / President’s Page Doug Bartlett DEPARTMENTS 02 / Letter From the Editor 04 / Sun ‘n Fun Speakers 26 / 2010 Regional Results THE COVER 30 / Contest Calendar and Advertisers Index Photo by Laurie Zaleski. 31 / FlyMart and Classifieds PHOTOGRAPHY COURTESY YUICHI TAGAKI REGGIE PAULK COMMENTARY / EDITOR’S LOG OFFICIAL MAGAZINE of the INTERNATIONAL AEROBATIC CLUB PUBLISHER: Doug Bartlett IAC MANAGER: Trish Deimer EDITOR: Reggie Paulk SENIOR ART DIRECTOR: Phil Norton DIRECTOR OF PUBLICATIONS: Mary Jones COPY EDITOR: Colleen Walsh CONTRIBUTING AUTHORS: Doug Bartlett John Morrissey Reggie Paulk Yuichi Tagaki Will Tyron Dave Watson IAC CORRESPONDENCE International Aerobatic Club, P.O. -
DCS: Su-27 Flanker Flight Manual
[SU-27] DCS DCS: Su-27 Flanker Eagle Dynamics i Flight Manual DCS [SU-27] DCS: Su-27 for DCS World The Su-27, NATO codename Flanker, is one of the pillars of modern-day Russian combat aviation. Built to counter the American F-15 Eagle, the Flanker is a twin-engine, supersonic, highly manoeuvrable air superiority fighter. The Flanker is equally capable of engaging targets well beyond visual range as it is in a dogfight given its amazing slow speed and high angle attack manoeuvrability. Using its radar and stealthy infrared search and track system, the Flanker can employ a wide array of radar and infrared guided missiles. The Flanker also includes a helmet-mounted sight that allows you to simply look at a target to lock it up! In addition to its powerful air-to-air capabilities, the Flanker can also be armed with bombs and unguided rockets to fulfil a secondary ground attack role. Su-27 for DCS World focuses on ease of use without complicated cockpit interaction, significantly reducing the learning curve. As such, Su-27 for DCS World features keyboard and joystick cockpit commands with a focus on the most mission critical of cockpit systems. General discussion forum: http://forums.eagle.ru ii [SU-27] DCS Table of Contents INTRODUCTION ........................................................................................................... VI SU-27 HISTORY ............................................................................................................. 2 ADVANCED FRONTLINE FIGHTER PROGRAMME ......................................................................... -
Chris Larson Soaring Over Michigan the “Remote” Instructor Bronze Badge Process Nutmeg Open House Ad
May, 2017 THE OFFICIAL PUBLICATION OF THE WOMEN SOARING PILOTS ASSOC. www.womensoaring.org IN THIS ISSUE PAGE 2 Badges June is WSPA dues’ renewal month President’s note Please pay on time From the Editor PAGE 4 Welcome new members Meet Chris Larson Virginia Gallenberger PAGE 5 My first solo WSPA committees PAGE 6 Famous women pilots: Melitta Schiller PAGE 7 100 years old woman celebrates her 100th birthday.. PAGE 8 Winter Soaring..Arizona Winter Soaing...Namibia This and That PAGE 9 NSM letter Shattered Dream A POH cannot be read too many times PAGE 10 Chris Larson soaring over Michigan The “remote” instructor Bronze Badge Process Nutmeg Open House ad PAGE 11 2017 WSPA Seminar page 2 May 2017 THE WOMEN SOARING PILOTS Badges ASSOCIATION (WSPA) WAS (reported through May 2017 A Badge FOUNDED IN 1986 AND IS Coleen Cameron, CO AFFILIATED WITH THE SOARING C Badge Maryam Ali, VA SOCIETY OF AMERICA Coleen Cameron, CO BOARD B Badge Mary Rust ,President Coleen Cameron, CO From the Editor 26630 Garret Ryan Ct. Recently, I got an e-mail from one of our members inquir- Hermet, CA 92544-6733 President’s Note ing why we need separate Charlotte Taylor, Vice President women contests or listing women Your newly elected WSPA Board Mem- 4206 JuniataSt. records separately. This also falls bers are off to a great start working on a St. Louis, MO 63116 into the category ‘why are there variety of projects! Though we have been so few women in aviation and in working on line together for 4 months, Joan Burn, Secretary soaring especially?’ WSPA and many of us have not met each other face 212 Marian Ct. -
Selig-2014-Jofac-Fli
JOURNAL OF AIRCRAFT Vol. 51, No. 6, November–December 2014 Real-Time Flight Simulation of Highly Maneuverable Unmanned Aerial Vehicles Michael S. Selig∗ University of Illinois at Urbana–Champaign, Urbana, Illinois 61801 DOI: 10.2514/1.C032370 This paper focuses on full six degree-of-freedom aerodynamic modeling of small unmanned aerial vehicles at high angles of attack and high sideslip in maneuvers performed using large control surfaces at large deflections for aircraft with high thrust-to-weight ratios. Configurations, such as this, include many of the currently available propeller- driven radio-controlled model airplanes that have control surfaces as large as 50% chord, deflections as high as 50 deg, and thrust-to-weight ratios near 2∶1. Airplanes with these capabilities are extremely maneuverable and aerobatic, and modeling their aerodynamic behavior requires new thinking because using traditional stability- derivative methods is not practical with highly nonlinear aerodynamic behavior and coupling in the presence of high prop-wash effects. The method described outlines a component-based approach capable of modeling these extremely maneuverable small unmanned aerial vehicles in a full six degree-of-freedom real-time environment over the full 180 deg range in angle of attack and sideslip. Piloted flight-simulation results for four radio-controlled/unmanned- aerial-vehicle configurations having wingspans in the range from 826 mm (32.5 in.) to 2540 mm (100 in.) are presented to highlight the results of the high-angle aerodynamic modeling approach. Maneuvers simulated include tailslides, knife-edge flight, high-angle upright and inverted flight, rolling maneuvers at high angle, and an inverted spin of a biplane. -
Unusual Attitudes and the Aerodynamics of Maneuvering Flight Author’S Note to Flightlab Students
Unusual Attitudes and the Aerodynamics of Maneuvering Flight Author’s Note to Flightlab Students The collection of documents assembled here, under the general title “Unusual Attitudes and the Aerodynamics of Maneuvering Flight,” covers a lot of ground. That’s because unusual-attitude training is the perfect occasion for aerodynamics training, and in turn depends on aerodynamics training for success. I don’t expect a pilot new to the subject to absorb everything here in one gulp. That’s not necessary; in fact, it would be beyond the call of duty for most—aspiring test pilots aside. But do give the contents a quick initial pass, if only to get the measure of what’s available and how it’s organized. Your flights will be more productive if you know where to go in the texts for additional background. Before we fly together, I suggest that you read the section called “Axes and Derivatives.” This will introduce you to the concept of the velocity vector and to the basic aircraft response modes. If you pick up a head of steam, go on to read “Two-Dimensional Aerodynamics.” This is mostly about how pressure patterns form over the surface of a wing during the generation of lift, and begins to suggest how changes in those patterns, visible to us through our wing tufts, affect control. If you catch any typos, or statements that you think are either unclear or simply preposterous, please let me know. Thanks. Bill Crawford ii Bill Crawford: WWW.FLIGHTLAB.NET Unusual Attitudes and the Aerodynamics of Maneuvering Flight © Flight Emergency & Advanced Maneuvers Training, Inc.