An Implementation of a Non-Monotonic Logic in an Embedded Computer for a Motor-Glider
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Advanced Coastal Navigation Coast Guard Auxiliary Association Inc. Washington, D. C. First Edition..........................................................................1987 Second Edition .....................................................................1990 Third Edition ........................................................................1999 Fourth Edition.......................................................................2002 ii iii iv v vi Advanced Coastal Navigation TABLE OF CONTENTS Introduction...................................................................................................ix Chapter 1 INTRODUCTION TO COASTAL NAVIGATION . .1-1 Chapter 2 THE MARINE MAGNETIC COMPASS . .2-1 Chapter 3 THE NAUTICAL CHART . .3-1 Chapter 4 THE NAVIGATOR’S TOOLS & INSTRUMENTS . .4-1 Chapter 5 DEAD RECKONING . .5-1 Chapter 6 PILOTING . .6-1 Chapter 7 CURRENT SAILING . .7-1 Chapter 8 TIDES AND TIDAL CURRENTS . .8-1 Chapter 9 RADIONAVIGATION . .9-1 Chapter 10 NAVIGATION REFERENCE PUBLICATIONS . .10-1 Chapter 11 FUEL AND VOYAGE PLANNING . .11-1 Chapter 12 REFLECTIONS . .12-1 Appendix A GLOSSARY . .A-1 INDEX . .Index-1 vii Advanced Coastal Navigation viii intRodUction WELCOME ABOARD! Welcome to the exciting world of completed the course. But it does marine navigation! This is the fourth require a professional atti tude, care- edition of the text Advanced Coastal ful attention to classroom presenta- Navigation (ACN), designed to be tions, and diligence in working out used in con cert with the 1210-Tr sample problems. chart in the Public Education (PE) The ACN course has been course of the same name taught by designed to utilize the 1210-Tr nau - the United States Coast Guard tical chart. It is suggested that this Auxiliary (USCGAUX). Portions of chart be readily at hand so that you this text are also used for the Basic can follow along as you read the Coastal Navigation (BCN) PE text. We recognize that students course. -
Answer Set Programming: a Primer?
Answer Set Programming: A Primer? Thomas Eiter1, Giovambattista Ianni2, and Thomas Krennwallner1 1 Institut fur¨ Informationssysteme, Technische Universitat¨ Wien Favoritenstraße 9-11, A-1040 Vienna, Austria feiter,[email protected] 2 Dipartimento di Matematica, Universita´ della Calabria, I-87036 Rende (CS), Italy [email protected] Abstract. Answer Set Programming (ASP) is a declarative problem solving para- digm, rooted in Logic Programming and Nonmonotonic Reasoning, which has been gaining increasing attention during the last years. This article is a gentle introduction to the subject; it starts with motivation and follows the historical development of the challenge of defining a semantics for logic programs with negation. It looks into positive programs over stratified programs to arbitrary programs, and then proceeds to extensions with two kinds of negation (named weak and strong negation), and disjunction in rule heads. The second part then considers the ASP paradigm itself, and describes the basic idea. It shows some programming techniques and briefly overviews Answer Set solvers. The third part is devoted to ASP in the context of the Semantic Web, presenting some formalisms and mentioning some applications in this area. The article concludes with issues of current and future ASP research. 1 Introduction Over the the last years, Answer Set Programming (ASP) [1–5] has emerged as a declar- ative problem solving paradigm that has its roots in Logic Programming and Non- monotonic Reasoning. This particular way of programming, in a language which is sometimes called AnsProlog (or simply A-Prolog) [6, 7], is well-suited for modeling and (automatically) solving problems which involve common sense reasoning: it has been fruitfully applied to a range of applications (for more details, see Section 6). -
Answer Set Programming with Default Logic
Answer Set Programming with Default Logic Victor W. Marek Jeffrey B. Remmel Department of Computer Science Department of Mathematics University of Kentucky University of California Lexington, KY 40506, USA, La Jolla, CA 92093, USA [email protected] [email protected] Abstract to be equivalent to Autoepistemic Logic of Moore (Moore 1985). See (Marek and Truszczynski´ 1993) for details. The We develop an Answer Set Programming formalism based basic complexity result for Default Logic was established by on Default Logic. We show that computing generating sets of Gottlob (Gottlob 1992) (see also Stillman (Stillman 1992). extensions in this formalism captures all ΣP search problems. 2 Gottlob found that the decision problems associated with the Default Logic are complete for the second level of polyno- I. Introduction mial hierarchy. Specifically, the existence problem for ex- P The main motivation for this paper comes from recent de- tensions is Σ2 complete, the membership problem for exten- sions (membership in some, membership in all) are com- velopments in knowledge representation theory. In partic- P P ular, a new generation of general solvers have been de- plete, respectively, for Σ2 and Π2 . veloped, (Niemela¨ and Simons 1996; Eiter et. al. 1998; A search problem ((Garey and Johnson 1979)) S has two Cholewinski´ et.al. 1999; Syrjanen 2001; Simons et. al. components. First, S specifies a set of finite instances 2002), based on the so-called Answer Set Programming (Garey and Johnson 1979). For example, the search prob- (ASP) paradigm (Niemela¨ 1998; Marek and Truszczynski´ lem may be to find Hamiltonian paths in a graph so that the 1999; Lifschitz 1999). -
FAA-H-8083-15, Instrument Flying Handbook -- 1 of 2
i ii Preface This Instrument Flying Handbook is designed for use by instrument flight instructors and pilots preparing for instrument rating tests. Instructors may find this handbook a valuable training aid as it includes basic reference material for knowledge testing and instrument flight training. Other Federal Aviation Administration (FAA) publications should be consulted for more detailed information on related topics. This handbook conforms to pilot training and certification concepts established by the FAA. There are different ways of teaching, as well as performing, flight procedures and maneuvers and many variations in the explanations of aerodynamic theories and principles. This handbook adopts selected methods and concepts for instrument flying. The discussion and explanations reflect the most commonly used practices and principles. Occasionally the word “must” or similar language is used where the desired action is deemed critical. The use of such language is not intended to add to, interpret, or relieve a duty imposed by Title 14 of the Code of Federal Regulations (14 CFR). All of the aeronautical knowledge and skills required to operate in instrument meteorological conditions (IMC) are detailed. Chapters are dedicated to human and aerodynamic factors affecting instrument flight, the flight instruments, attitude instrument flying for airplanes, basic flight maneuvers used in IMC, attitude instrument flying for helicopters, navigation systems, the National Airspace System (NAS), the air traffic control (ATC) system, instrument flight rules (IFR) flight procedures, and IFR emergencies. Clearance shorthand and an integrated instrument lesson guide are also included. This handbook supersedes Advisory Circular (AC) 61-27C, Instrument Flying Handbook, which was revised in 1980. -
Flight Instruments - Rev
Flight Instruments - rev. 9/12/07 Ground Lesson: Flight Instruments Objectives: 1. to understand the flight instruments, and the systems that drive them 2. to understand the pitot static system, and possible erroneous behavior 3. to understand the gyroscopic instruments 4. to understand the magnetic instrument, and the short comings of the instrument Justification: 1. understanding of flight instruments is critical to evaluating proper response in case of failure 2. knowledge of flight instruments is required for the private pilot checkride. Schedule: Activity Est. Time Ground 1.0 Total 1.0 Elements Ground: • overview • pitot-static instruments • gyroscopic instruments • magnetic instrument Completion Standards: 1. when the student exhibits knowledge relating to flight instruments including their failure symptoms 1 of 3 Flight Instruments - rev. 9/12/07 Presentation Ground: pitot-static system 1. overview (1) pitot-static system uses ram- air and static air measurements to produce readings. (2) pressure and temperature effect the altimeter i. remember - “Higher temp or pressure = Higher altitude” ii. altimeters are usually adjustable for non-standard temperatures via a window in the instrument (i) 1” of pressure difference is equal to approximately 1000’ of altitude difference 2. components (1) static ports (2) pitot tube (3) pitot heat (4) alternate static ports (5) instruments - altimeter, airspeed, VSI gyroscopic system 1. overview (1) vacuum :system to allow high-speed air to spin certain gyroscopic instruments (2) typically vacuum engine-driven for some instruments, AND electrically driven for other instruments, to allow back-up in case of system failure (3) gyroscopic principles: i. rigidity in space - gyroscopes remains in a fixed position in the plane in which it is spinning ii. -
Stable Models Stable Models (‘Answer Sets’) for a Normal Logic Program, a Stable Model Is a Set of Atoms
491 Knowledge Representation Stable models Stable models (‘Answer sets’) For a normal logic program, a stable model is a set of atoms. Let P be a ground normal logic program, i.e., one without variables. If P is not ground Marek Sergot (contains variables) then replace it by all the ground instances of its clauses. (The resulting Department of Computing set of clauses may not be finite.) Imperial College, London Notation When r is a (ground) clause of the form: February 2006 v1.2, November 2016 v1.2c A B ,...,B , not C ,..., not C ← 1 m 1 n + head(r) = A, body (r) = B1,...,Bm , body−(r) = C1,...,Cn . When P is a set of A normal logic program (sometimes a ‘general logic program’) is a set of clauses of the clauses, heads(P ) = head({r) r P .} { } form: { | ∈ } Suppose we have a set X of atoms from the language of P . The idea is that we use X to A L ,...,L (n 0) ← 1 n ≥ simplify P by ‘partially evaluating’ all clauses with nbf-literals against X, and then we see whether the simplified program P X we are left with (the ‘reduct’) has a least Herbrand where A is an atom and each Li is either an atom or a nbf-literal of the form not A where A is an atom. not denotes negation by failure. model that coincides with X. A model of a normal logic program P is a set of atoms X such that T (X) X, or P ⊆ equivalently, such that X is an (ordinary, classical) model of the clauses P ¬ obtained by Definition replacing every occurrence of not in P by ordinary, truth-functional negation . -
ASA Ch 3 the Instrument - Workbook Questions
ASA Ch 3 The Instrument - Workbook Questions 1. The flight instruments are commonly grouped into basic categories based on the a. physical properties they rely on to work. b. whether they are used on the ground or in flight. c. Library of Congress catalog system, Dewey Decimal. 2. The basis of a conventional attitude indicator is a self-erecting a. vertical card mounted on a swivel. b. attitude flag arranged on a diagonal. c. gyroscope spinning on a vertical axis. 3. If the spin axis of the attitude indicator gyroscope moves off the vertical for some reason, the internal mechanism will realign it at a rate of approximately a. 3 degrees per second. b. 3 degrees per minute. c. 3 degrees per hour. 4. Occasionally, the miniature airplane on the attitude indicator may require repositioning while in level flight, due to changes in a. altitude (and corresponding air density). b. pitch attitude (associated with airspeed changes). c. the Earth’s gravitational forces. 5. If the attitude indicator experiences a failure of the power source, it will a. be unusable. b. continue to function if you maintain the same heading. c. still be a valid source of bank attitude. 6. Acceleration of the aircraft may cause the gyroscope to move off vertical, moving the horizon line a. toward the pilot. b. in the direction of the turn. c. to an incorrect position. 7. During a rapid acceleration, the horizon line will move down and the attitude indicator will indicate a false climb. a. True b. False 8. To avoid false indications when speeding up or slowing down, a pilot should increase the instrument scan rate a. -
Finish Your Private Pilot License
THE PRIVATE PILOT LEARNING GUIDE STOPPING A TURN CARDINAL DIRECTIONS Coordinated aileron and rudder pressure in the direction opposite When referencing the magnetic compass or heading indicator, always TURNS the bank will return the airplane to a level attitude. As with the associate one of the eight cardinal directions with the number on roll in the roll out of a bank attitude requires rudder deflection to the indicator. This will assist you in keeping spatially oriented and overcome adverse yaw. Relax elevator back pressure to return to a will be very important later in your training when you must visualize Rolling the airplane into a banked attitude results in a turn. Since the flight path is now curved there is an level pitch attitude as the bank attitude decreases. Neutralize the runway directions and while doing cross country navigation. controls when reaching a level sight picture. acceleration force. The increased force is directly related to the bank attitude used for the turn. A shallow As an aircraft rotates about its longitudinal axis, the lifting force bank attitude results in a slowly changing flight path, creating only a small increase in load factor. also rotates remaining perpendicular to the wingspan. When the airplane is in a bank, this redirected lift causes the airplane to turn. 60o As discussed earlier in this chapter, turning results in a curved flight path and additional load. The increase in load is due to centrifugal 40o force and is present anytime the airplane is turning. The centrifugal force combines with the airplane’s weight resulting in “load” opposite to lift. -
Arxiv:1905.04725V1
Sequent-Type Proof Systems for Three-Valued Default Logic⋆ Sopo Pkhakadze Institute of Logic and Computation, Knowledge-Based Systems Group E192-03, Technische Universität Wien, Favoritenstraße 9-11, 1040 Vienna, Austria ORCID ID: 0000-0003-2247-8147 [email protected] Abstract. Sequent-type proof systems constitute an important and widely-used class of calculi well-suited for analysing proof search. In my master’s thesis, I in- troduce sequent-type calculi for a variant of default logic employing Łukasiewicz’s three-valued logic as the underlying base logic. This version of default logic has been introduced by Radzikowska addressing some representational shortcomings of standard default logic. More specifically, the calculi discussed in my thesis axiomatise brave and skeptical reasoning for this version of default logic, respec- tively following the sequent method first introduced in the context of nonmono- tonic reasoning by Bonatti and Olivetti, which employ a complementary calculus for axiomatising invalid formulas, taking care of expressing the consistency con- dition of defaults. 1 Background Nonmonotonicreasoning is a well-established area in knowledge representation and rea- soning dealing with formalisations of rational arguments whose characteristic feature is that their conclusions may have to be retracted in the light of new, more specific infor- mation. Thus, the inference mechanism underlying rational arguments is nonmonotonic in the sense that an increased set of premisses does not necessarily entail an increased set of conclusions. This is in contradistinction to valid arguments whose underlying in- arXiv:1905.04725v1 [cs.LO] 12 May 2019 ference process is monotonic. Many different nonmonotonic formalisms have been in- troduced in the literature, most prominent among them are default logic [39], autoepis- temic logic [34], circumscription [32], and logic programming under the answer-set semantics [20,21]. -
The Inertial Navigation Unit: Teaching Navigation Principles Using a Custom Designed Sensor Package
AC 2008-755: THE INERTIAL NAVIGATION UNIT: TEACHING NAVIGATION PRINCIPLES USING A CUSTOM DESIGNED SENSOR PACKAGE Joe Bradshaw, U.S. Naval Academy Electronics Technician at the US Naval Academy for the Weapons and Systems Engineering Department for 7 years. Design special hardware and develop software for projects and labs. Jack Nicholson, U.S. Naval Academy Page 13.1241.1 Page © American Society for Engineering Education, 2008 The Inertial Navigation Unit: Teaching Navigation Principles using a Custom Designed Sensor Package Abstract This paper describes the application and design of a small, inexpensive inertial navigation unit (INU) created to introduce systems engineering students at the United States Naval Academy (USNA) to the principles of navigation systems and to act as a navigation sensor for robotic and autonomous vehicle projects. The INU has been used in place of a multitude of standard navigation sensors such as an inertial measurement unit (IMU), magnetic compass module, and Global Positioning System (GPS) receiver. Its integrated design simplifies mechanical mounting, reduces navigation system weight and size, simplifies data interfacing with a control computer, and provides great flexibility for reconfiguring to meet a variety of engineering education objectives. The INU is capable of firmware upgrades and algorithm enhancements in the field via in-circuit programming, enhancing its longevity as a useful educational tool. In addition, a variety of controllers or a personal computer (PC) can communicate with the INU board through a standard RS-232C serial interface. This compact unit provides good system performance at a reasonable cost compared to most commercially available units. These features enable hands-on education techniques in the navigation aspects of robotics, examples of which are presented. -
What Is Answer Set Programming?
What Is Answer Set Programming? Vladimir Lifschitz Department of Computer Sciences University of Texas at Austin 1 University Station C0500 Austin, TX 78712 [email protected] Abstract Their approach is based on the relationship between plans and stable models described in (Subrahmanian & Zaniolo Answer set programming (ASP) is a form of declarative pro- 1995). Soininen & Niemel¨a(1998) applied what is now gramming oriented towards difficult search problems. As an outgrowth of research on the use of nonmonotonic reason- known as answer set programming to the problem of prod- ing in knowledge representation, it is particularly useful in uct configuration. The use of answer set solvers for search knowledge-intensive applications. ASP programs consist of was identified as a new programming paradigm in (Marek rules that look like Prolog rules, but the computational mech- & Truszczy´nski 1999) (the term “answer set programming” anisms used in ASP are different: they are based on the ideas was used for the first time as the title of a part of the collec- that have led to the creation of fast satisfiability solvers for tion where that paper appeared) and in (Niemel¨a1999). propositional logic. An answer set programming language Introduction System LPARSE was originally created as a front-end for the 3 Answer set programming (ASP) is a form of declarative answer set solver SMODELS, and it is now used in the same 4 programming oriented towards difficult, primarily NP-hard, way in most other answer set solvers. search problems. As an outgrowth of research on the use Some rules found in LPARSE programs are traditional of nonmonotonic reasoning in knowledge representation, it “Prolog-style” rules, such as is particularly useful in knowledge-intensive applications. -
1 Altimeter and Compass Watch Instruction Manual Overview Features • Hour, Minute, Second, Year, Month, Day, Day of Week •
Altimeter and Compass Watch Instruction Manual Overview Figure 1 LCD display description Features • Hour, minute, second, year, • Auto calendar • 12/24 hour format display month, day, day of week • Daily alarm • Dual time • Stopwatch • Difference measurement of • Countdown timer • Altimeter – Barometer Use Altimeter and Barometer • 24 hour memory in • Logbook and logbook • 4 day memory in Barometer Altimeter history • Current absolute • Sea level pressure • Temperature display atmospheric • Electro – luminescent back • Compass • Low battery indicator lighted LCD • Diagnostics (System Reset) Care and Maintenance • Protect your watch from shocks, extreme heat and directly exposure to sunlight. • Don’t try to remove the housing or button of the watch. • Don’t insert any object into the watch. • Always put the watch in a clear, dry and room temperature environment when the watch is not used. • Follow the procedure discussed in the manual only. • Make sure the area around the sensors is free of dust or strong chemical. 1 Quick Reference Guide Figure 2 Quick Reference Guide 2 Time Time Main Mode Path Press (S1) until the mode indicator points to the “TIME” Field 1 Day of week, barometer trend indicator Field 2 Hour, Minute, Second Field 3 Month, day Second animation Outer Circumference Adjust o Hold (S2) for 1 second, the second digit will begin to flash o Press (S2) to select second minute hour 12/24hour year month day o Press (S3) or (S4) to set the function o Press (S1) to accept the setting Daily Alarm Path Press (S2) ×1 from Time Main Mode Field 1 “ON” or “OFF” Field 2 Time of a particular alarm Current time Field 3 Adjust o Press (S3) or (S4) to select the alarm number o Hold (S2) for 1 second, the “ON” or “OFF” will begin to flash o Press (S2) to select “ON” or “OFF” hour minute o Press (S3) or (S4) to set the function o Press (S1) to accept the setting Note “ ” will be displayed when any alarm is enabled.