• 제목/요약/키워드: Integral Attack

검색결과 20건 처리시간 0.025초

경량 블록 암호 PIPO의 MILP-Aided 디비전 프로퍼티 분석 및 인테그랄 공격 (MILP-Aided Division Property and Integral Attack on Lightweight Block Cipher PIPO)

  • 김제성;김성겸;김선엽;홍득조;성재철;홍석희
    • 정보보호학회논문지
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    • 제31권5호
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    • pp.875-888
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    • 2021
  • 본 논문에서는 경량 블록 암호 PIPO에 대한 인테그랄 구별자(integral distinguisher)을 탐색한 결과를 통해 8-라운드 PIPO-64/128에 대한 키 복구 공격을 수행한다. ICISC 2020에서 제안된 경량 블록 암호 PIPO는 고차 마스킹 구현을 고려한 설계를 통해 부채널 공격에 대한 저항성을 갖는 효율적인 구현이 가능하다. 동시에 차분 분석, 선형 분석 등의 다양한 분석법을 적용하여 PIPO의 안전성을 보였다. 그러나 인테그랄 공격에 대해, 5-라운드 이상의 인테그랄 구별자가 존재하지 않을 것이라고 제안되었을 뿐 인테그랄 공격에 대한 안전성 분석은 현재까지 수행된 바 없다. 본 논문에서는 MILP 기반 Division Property를 통해 PIPO에 대한 인테그랄 구별자를 탐색하는 방법을 제시하고, 기존의 결과와 달리 6-라운드 인테그랄 구별자가 존재함을 보인다. 뿐만 아니라, PIPO의 라운드 함수 구조를 활용하여 입출력에 대한 선형 변환을 고려하는 인테그랄 구별자 탐색 방법을 통해 총 136개의 6-라운드 인테그랄 구별자를 제시한다. 마지막으로, 획득한 6-라운드 인테그랄 구별자 중 4개를 이용하여 2124.5849의 시간 복잡도와 293의 메모리 복잡도를 가지는 8-라운드 PIPO-64/128 키 복구 공격을 제안한다.

비밀 S-box를 사용한 GFN에 대한 안전성 분석 (Security Analysis on GFN with Secret S-box)

  • 이용성;강형철;홍득조;성재철;홍석희
    • 정보보호학회논문지
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    • 제27권3호
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    • pp.467-476
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    • 2017
  • 본 논문에서는 라운드 함수의 업데이트 함수로 SP 구조를 사용하고 비밀 S-box가 적용된 GFN(Generalized Feistel Networks) Type I, Type II, Type III에 대한 안전성을 분석한다. 이 환경에서 공격자는 S-box에 대한 정보를 갖지 못한다. 인테그랄 공격 기법(Integral attack) 기반의 선택 평문 공격으로 9 라운드(Type I), 6 라운드(Type II), 6라운드(Type III)에 대한 비밀 S-box 정보를 복구할 수 있다. 선택 암호문 공격으로 전환할 경우 GFN Type I의 16 라운드까지 비밀 S-box의 정보가 복구된다. 결론적으로 m비트 비밀 S-box와 $k{\times}k$ MDS 행렬이 라운드 함수로 사용된 GFN Type I, Type II, Type III에 대하여 비밀 S-box를 복구하는데 ${\frac{2^{3m}}{32k}},{\frac{2^{3m}}{24k}},{\frac{2^{3m}}{36k}}$만큼의 시간복잡도가 필요하다.

SQP와 CEALM 최적화 기법에 의한 대공 방어 유도탄에 대한 3차원 최적 회피 성능 비교 (Performance Comparison of 3-D Optimal Evasion against PN Guided Defense Missiles Using SQP and CEALM Optimization Methods)

  • 조성봉;유창경;탁민제
    • 한국군사과학기술학회지
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    • 제12권3호
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    • pp.272-281
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    • 2009
  • In this paper, three-dimensional optimal evasive maneuver patterns for air-to-surface attack missiles against proportionally navigated anti-air defense missiles were investigated. An interception error of the defense missile is produced by an evasive maneuver of the attack missile. It is assumed that the defense missiles are continuously launched during the flight of attack missile. The performance index to be minimized is then defined as the negative square integral of the interception errors. The direct parameter optimization technique based on SQP and a co-evolution method based on the augmented Lagrangian formulation are adopted to get the attack missile's optimal evasive maneuver patterns. The overall shape of the resultant optimal evasive maneuver is represented as a deformed barrel-roll.

Remaining service life estimation of reinforced concrete buildings based on fuzzy approach

  • Cho, Hae-Chang;Lee, Deuck Hang;Ju, Hyunjin;Kim, Kang Su;Kim, Ki-Hyun;Monteiro, Paulo J.M.
    • Computers and Concrete
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    • 제15권6호
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    • pp.879-902
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    • 2015
  • The remaining service life (RSL) of buildings has been an important issue in the field of building and facility management, and its development is also one of the essential factors for achieving sustainable infrastructure. Since the estimation of RSL of buildings is heavily affected by the subjectivity of individual inspector or engineer, much effort has been placed in the development of a rational method that can estimate the RSL of existing buildings more quantitatively using objective measurement indices. Various uncertain factors contribute to the deterioration of the structural performance of buildings, and most of the common building structures are constructed not with a single structural member but with various types of structural components (e.g., beams, slabs, and columns) in multistory floors. Most existing RSL estimation methods, however, consider only an individual factor. In this study, an estimation method for RSL of concrete buildings is presented by utilizing a fuzzy theory to consider the effects of multiple influencing factors on the deterioration of durability (e.g., concrete carbonation, chloride attack, sulfate attack), as well as the current structural condition (or damage level) of buildings.

A Study on Longitudinal Phugoid Mode Affected by Application of Nonlinear Control Laws

  • Kim, Chong-Sup;Hur, Gi-Bong;Kim, Seung-Jun
    • International Journal of Aeronautical and Space Sciences
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    • 제8권1호
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    • pp.21-31
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    • 2007
  • Relaxed Static Stability (RSS) concept has been applied to improve aerodynamic performance of modern version supersonic jet fighter aircraft. The T-50 advanced supersonic trainer employs the RSS concept in order to improve the aerodynamic performance. And the flight control system stabilizes the unstable aircraft and provides adequate handling qualities. The T-50 longitudinal control laws employ a proportional-plus-integral type controller based on a dynamic inversion method. The longitudinal dynamic modes consist of short period with high frequency and phugoid mode with low frequency. The design goal of longitudinal control law is optimization of short period damping ratio and frequency using Lower Order Equivalent System (LOES) complying the requirement of MIL-F-8785C. This paper addresses phugoid mode characteristics such as damping ratio and natural frequency that is affected by the nonlinear control laws such as angle of attack limiter, auto pitch attitude command system and autopilot of pitch attitude hold.

FUZZY CONTROL LAW OF HIGHLY MANEUVERABLE HIGH PERFORMANCE AIRCRAFT

  • Sul Cho;Park, Rai-Woong;Nam, Sae-Kyu;Lee, Man-Hyung
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1998년도 제13차 학술회의논문집
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    • pp.205-209
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    • 1998
  • A synthesis of fuzzy variable structure control is proposed to design a high-angle-of-attack flight system for a modification version of the F-18 aircraft. The knowledge of the proportional, integral, and derivative control is combined into the fuzzy control that addresses both the highly nonlinear aerodynamic characteristics of elevators and the control limit of thrust vectoring nozzles. A simple gain scheduling method with multi-layered fuzzy rules is adopted to obtain an appropriate blend of elevator and thrust vectoring commands in the wide operating range. Improving the computational efficiency, an accelerated kernel for on-line fuzzy reasoning is also proposed. The resulting control system achieves the good flying quantities during a high-angle-of- attack excursion. Thus the fuzzy logic can afford the control engineer a flexible means of deriving effective control laws in the nonlinear flight regime.

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A DDoS attack Mitigation in IoT Communications Using Machine Learning

  • Hailye Tekleselase
    • International Journal of Computer Science & Network Security
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    • 제24권4호
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    • pp.170-178
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    • 2024
  • Through the growth of the fifth-generation networks and artificial intelligence technologies, new threats and challenges have appeared to wireless communication system, especially in cybersecurity. And IoT networks are gradually attractive stages for introduction of DDoS attacks due to integral frailer security and resource-constrained nature of IoT devices. This paper emphases on detecting DDoS attack in wireless networks by categorizing inward network packets on the transport layer as either "abnormal" or "normal" using the integration of machine learning algorithms knowledge-based system. In this paper, deep learning algorithms and CNN were autonomously trained for mitigating DDoS attacks. This paper lays importance on misuse based DDOS attacks which comprise TCP SYN-Flood and ICMP flood. The researcher uses CICIDS2017 and NSL-KDD dataset in training and testing the algorithms (model) while the experimentation phase. accuracy score is used to measure the classification performance of the four algorithms. the results display that the 99.93 performance is recorded.

An Improved Pseudorandom Sequence Generator and its Application to Image Encryption

  • Sinha, Keshav;Paul, Partha;Amritanjali, Amritanjali
    • KSII Transactions on Internet and Information Systems (TIIS)
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    • 제16권4호
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    • pp.1307-1329
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    • 2022
  • This paper proposes an improved Pseudorandom Sequence Generator (PRSG) based on the concept of modular arithmetic systems with non-integral numbers. The generated random sequence use in various cryptographic applications due to its unpredictability. Here the mathematical model is designed to solve the problem of the non-uniform distribution of the sequences. In addition, PRSG has passed the standard statistical and empirical tests, which shows that the proposed generator has good statistical characteristics. Finally, image encryption has been performed based on the sort-index method and diffusion processing to obtain the encrypted image. After a thorough evaluation of encryption performance, there has been no direct association between the original and encrypted images. The results show that the proposed PRSG has good statistical characteristics and security performance in cryptographic applications.

통합보안관리 에이전트를 확장한 웹 어플리케이션 공격 탐지 연구 (A Study of Web Application Attack Detection extended ESM Agent)

  • 김성락
    • 한국컴퓨터정보학회논문지
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    • 제12권1호
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    • pp.161-168
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    • 2007
  • 웹에 대한 공격은 웹 서버 자체의 취약점 보다 웹 어플리케이션의 구조, 논리, 코딩상의 오류를 이용한다. OWASP에서 웹 어플리케이션 취약점을 10가지로 분류하여 발표한 자료에 의하면 웹 해킹의 위험성과 피해가 심각함을 잘 알 수 있다. 이에 따라 웹 해킹에 대한 탐지능력 및 대응이 절실히 요구된다. 이러한 웹 공격을 방어하기 위해 패턴 매칭을 이용한 필터링을 수행하거나 코드를 수정하는 방법이 있을 수 있지만 새로운 공격에 대해서는 탐지 및 방어가 어렵다. 또한 침입탐지시스템이나 웹 방화벽과 같은 단위보안 제품을 도입할 수 있지만 운영과 지속적인 유지를 위해서는 많은 비용과 노력이 요구되며 많은 탐지의 오류를 발생한다. 본 연구에서는 웹 어플리케이션의 구조와 파라미터 입력 값에 대한 타입, 길이와 같은 특성 값들을 추출하는 프로파일링 기법을 이용하여 사전에 웹 어플리케이션 구조 데이터베이스를 구축함으로서 사용자 입력 값 검증의 부재에 대한 해결과 비정상적인 요청에 대해 데이터베이스의 프로파일 식별자를 이용하여 검증하고 공격 탐지가 가능하다. 통합보안관리시스템은 현재 대부분 조직에서 도입하여 운영하고 있으며 일반화 되어있다. 그래서 통합보안관리시스템의 보안 감사 로그 수집 에이전트에 웹 어플리케이션 공격 탐지 기능을 추가한 모델을 제시함으로서 추가 단위보안제품을 도입하지 않고서도 웹 어플리케이션 공격을 탐지할 수 있도록 하였다.

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Development of Flight Control Laws for the T-50 Advanced Supersonic Jet Trainer

  • Kim, Chong-Sup;Hur, Gi-Bong;Hwang, Byung-Moon;Cho, In-Je;Kim, Seung-Jun
    • International Journal of Aeronautical and Space Sciences
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    • 제8권1호
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    • pp.32-45
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    • 2007
  • The T-50 advanced supersonic jet trainer employs the Relaxed Static Stability (RSS) concept to improve the aerodynamic performance while the flight control system stabilizes the unstable aircraft and provides adequate handling qualities. The T-50 flight control laws employ a proportional-plus-integral type controller based on a dynamic inversion method in longitudinal axis and a proportional type controller based on a blended roll system with simple roll rate feedback and beta-betadot feedback system. These control laws are verified by flight tests with various maneuver set flight envelopes and the control laws are updated to resolve flight test issues. This paper describes several concepts of flight control laws used in T-50 to resolve those flight test issues. Control laws for solving the roll-off problem during pitch maneuver in asymmetric loading configurations, improving the departure resistance in negative angle of attack conditions and enhancing the fine tracking performance in air-to-air tracking maneuvers are described with flight test data.