• 제목/요약/키워드: State-Space

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Spaceborne Gravity Sensors for Continental Hydrology and Geodynamic Studies

  • Shum C. K.;Han Shin-Chan;Braun Alexander
    • 대한원격탐사학회지
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    • 제21권1호
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    • pp.51-57
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    • 2005
  • The currently operating NASA/GFZ Gravity Recovery and Climate Experiment (GRACE) mission is designed to measure small mass changes over a large spatial scale, including the mapping of continental water storage changes and other geophysical signals in the form of monthly temporal gravity field. The European Space Agency's Gravity field and steady state Ocean Circulation Explorer (GOCE) space gravity gradiometer (SGG) mission is anticipated to determine the mean Earth gravity field with an unprecedented geoid accuracy of several cm (rms) with wavelength of 130km or longer. In this paper, we present a summary of present GRACE studies for the recovery of hydrological signals in the Amazon basin using alternative processing and filtering techniques, and local inversion to enhance the temporal and spatial resolutions by two-folds or better. Simulation studies for the potential GRACE detection of slow deformations due to Nazca-South America plate convergence and glacial isostatic adjustment (GIA) signals show that these signals are at present difficult to detect without long-term data averaging and further improvement of GRACE measurement accuracy.

우주법상 손해배상책임과 분쟁해결제도 (The Liability for Damage and Dispute Settlement Mechanism under the Space Law)

  • 이강빈
    • 한국중재학회지:중재연구
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    • 제20권2호
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    • pp.173-198
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    • 2010
  • The purpose of this paper is to research on the liability for the space damage and the settlement of the dispute with reference to the space activity under the international space treaty and national space law of Korea. The United Nations has adopted five treaties relating to the space activity as follows: The Outer Space Treaty of 1967, the Rescue and Return Agreement of 1968, the Liability Convention of 1972, the Registration Convention of 1974, and the Moon Treaty of 1979. All five treaties have come into force. Korea has ratified above four treaties except the Moon Treaty. Korea has enacted three national legislations relating to space development as follows: Aerospace Industry Development Promotion Act of 1987, Outer Space Development Promotion Act of 2005, Outer Space Damage Compensation Act of 2008. The Outer Space Treaty of 1967 regulates the international responsibility for national activities in outer space, the national tort liability for damage by space launching object, the national measures for dispute prevention and international consultation in the exploration and use of outer space, the joint resolution of practical questions by international inter-governmental organizations in the exploration and use of outer space. The Liability Convention of 1972 regulates the absolute liability by a launching state, the faulty liability by a launching state, the joint and several liability by a launching state, the person claiming for compensation, the claim method for compensation, the claim period of compensation, the claim for compensation and local remedy, the compensation amount for damage by a launching state, the establishment of the Claims Commission. The Outer Space Damage Compensation Act of 2008 in Korea regulates the definition of space damage, the relation of the Outer Space Damage Compensation Act and the international treaty, the non-faulty liability for damage by a launching person, the concentration of liability and recourse by a launching person, the exclusion of application of the Product Liability Act, the limit amount of the liability for damage by a launching person, the cover of the liability insurance by a launching person, the measures and assistance by the government in case of occurring the space damage, the exercise period of the claim right of compensation for damage. The Liability Convention of 1972 should be improved as follows: the problem in respect of the claimer of compensation for damage, the problem in respect of the efficiency of decision by the Claims Commission. The Outer Space Damage Compensation Act of 2008 in Korea should be improved as follows: the inclusion of indirect damage into the definition of space damage, the change of currency unit of the limit amount of liability for damage, the establishment of joint and several liability and recourse right for damage by space joint launching person, the establishment of the Space Damage Compensation Review Commission. The 1998 Final Draft Convention on the Settlement of Disputes Related to Space Activities of 1998 by ILA regulates the binding procedure and non-binding settlement procedure for the disputes in respect of space activity. The non-binding procedure regulates the negotiation or the peaceful means and compromise for dispute settlement. The binding procedure regulates the choice of a means among the following means: International Space Law Court if it will be established, International Court of Justice, and Arbitration Court. The above final Draft Convention by ILA will be a model for the innovative development in respect of the peaceful settlement of disputes with reference to space activity and will be useful for establishing the frame of practicable dispute settlement. Korea has built the space center at Oinarodo, Goheung Province in June 2009. Korea has launched the first small launch vehicle KSLV-1 at the Naro Space Center in August 2009 and June 2010. In Korea, it will be the possibility to be occurred the problems relating to the international responsibility and dispute settlement, and the liability for space damage in the course of space activity. Accordingly the Korean government and launching organization should make the legal and systematic policy to cope with such problems.

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우주활동에 의하여 발생한 손해배상책임에 관한 연구 - 관련 사례를 중심으로 - (A Study on the Liability for Damage caused by Space Activity - With reference to Relevant Cases -)

  • 이강빈
    • 항공우주정책ㆍ법학회지
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    • 제26권1호
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    • pp.177-213
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    • 2011
  • 현재 우주활동에 의하여 발생된 손해에 대한 배상책임과 관련된 국제조약으로 1967년 우주조약과 1972년 우주손해배상책임조약이 있으며, 또한 우리나라 국내법으로 2008년 우주손해배상법이 있다. 우주조약은 우주활동에 대한 국가의 국제적 책임과 우주물체에 의한 손해에 대한 국가의 불법행위 책임에 관하여 규정하고 있다. 우주손해책임조약은 발사국의 절대적 책임, 과실책임, 연대책임, 배상청구권자, 배상청구방법, 배상청구기한, 배상청구와 국내적 구제, 손해배상액, 청구위원회 설치 등에 관하여 규정하고 있다. 우리나라 우주손해배상법은 우주손해의 정의, 우주손해책임조약과의 관계, 발사자의 무과실책임 및 책임의 집중, 발사자의 손해배상책임한도액, 발사자의 책임보험 가입, 정부의 피해자 구조 및 발사자 지원 등에 관하여 규정하고 있다. 우주사고로 인한 손해배상책임 관련 사례들로 Iridium33과 Cosmos 2251 위성충돌 사건, Cosmos 954 위성추락 사건, Martin Marietta의 위성발사 실패 사건, Westar VI 위성 작동불량 사고 등이 있으며, 이러한 우주사건에 관한 분쟁 또는 소송에 있어서 위성의 발사국, 발사자 및 제조자의 손해배상책임 부담문제에 관련하여 절대책임(엄격책임)원칙 또는 과실책임원칙이 적용되어 해결되고 있다. 우주손해책임조약의 개선방안으로 손해배상청구권자의 명확한 규정, 청구위원회의 결정의 구속력 확보 등을 들 수 있고, 우리나라 우주손해배상법의 개선방안으로 손해배상범위에 간접손해 포함, 손해배상책임 한도액의 통화단위 변경, 공동발사자의 연대책임 및 구상권 신설, 우주손해배상심의위원회의 설치 등을 들 수 있다. 우리나라는 2009년 6월 전남 고흥군 외나로도에 우주센터가 준공되어 동년 8월 및 2010년 6월 우리나라 최초 소형 우주발사체 나로호(KSLV-1)를 두차례 발사하였다. 향후 우리나라는 우주활동 과정에서 우주관련 국제조약 및 국내법상의 국제적 책임 및 우주손해에 대한 배상책임 등 문제들이 발생할 가능성이 있으므로 우리정부 및 우주물체 발사기관은 이러한 문제들에 대한 법적 제도적 대응책을 마련해야 할 것이다.

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최적 유한 임펄스 응답 평활기를 이용한 미지 입력 추정 기법 (Unknown Input Estimation using the Optimal FIR Smoother)

  • 권보규
    • 제어로봇시스템학회논문지
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    • 제20권2호
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    • pp.170-174
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    • 2014
  • In this paper, an unknown input estimation method via the optimal FIR smoother is proposed for linear discrete-time systems. The unknown inputs are represented by random walk processes and treated as auxiliary states in augmented state space models. In order to estimate augmented states which include unknown inputs, the optimal FIR smoother is applied to the augmented state space model. Since the optimal FIR smoother is unbiased and independent of any a priori information of the augmented state, the estimates of each unknown input are independent of the initial state and of other unknown inputs. Moreover, the proposed method can be applied to stochastic singular systems, since the optimal FIR smoother is derived without the assumption that the system matrix is nonsingular. A numerical example is given to show the performance of the proposed estimation method.

Layered Classifier System by Classification of Environment

  • Kim, Ji-Yoon;Lee, Dong-Wook;Sim, Kwee-Bo
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2003년도 ICCAS
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    • pp.1517-1520
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    • 2003
  • Generally, the environment we want to apply classifier system to is composed of several state spaces. So in this paper, we propose the layered classifier system having multifarious rule bases. From sensor's inputs, the lower layer of the layered classifier system learns strategies for each environmental state space. The higher layer learns how to allot each rule base of the strategy for environmental state space properly. To evaluate the proposed architecture of classifier system, we designed virtual environment having multifarious state spaces and from the analysis of the experimental results, we affirm that layered classifier system could find better strategies during a little time than other established classifier system's findings.

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The Solution for Cooperative Beamforming Design in MIMO Multi-way Relay Networks

  • Wang, Yong;Wu, Hao;Tang, Liyang;Li, Hui
    • KSII Transactions on Internet and Information Systems (TIIS)
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    • 제9권3호
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    • pp.956-970
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    • 2015
  • In this paper, we study the design of network coding for the generalized transmit scheme in multiple input multiple output Y channel, where K users wish to exchange specified and shared information with each other within two slots. Signal space alignment at each user and the relay is carefully constructed to ensure that the signals from the same user pair are grouped together. The cross-pair interference can be canceled during both multiple accessing channel phase and broadcasting channel phase. The proposed signal processing scheme achieves the degrees of freedom of ${\eta}(K)=K^2$ with fewer user antennas.

입출력 부공간에서의 데이터 클러스터링에 의한 퍼지제어 시스템 설계 (Fuzzy control system design by data clustering in the input-output subspaces)

  • 김민수;공성곤
    • 전자공학회논문지S
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    • 제34S권12호
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    • pp.30-40
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    • 1997
  • This paper presents a design method of fuzzy control systems by clustering the data in the subspace of the input-output produyct space. In the case of servo control, most input-outputdata are concentrated in thye steady-state region, and the the clustering will result in only steady-state fuzzy rules. To overcome this problem, we divide the input-output product space into some subspaces according to the state of input variables. The fuzzy control system designed by the subspace clustering showed good transient response and smaller steady-state error, which is comparable with the reference fuzzy system.

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Reinforcement Leaming Using a State Partition Method under Real Environment

  • Saito, Ken;Masuda, Shiro;Yamaguchi, Toru
    • 한국지능시스템학회:학술대회논문집
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    • 한국퍼지및지능시스템학회 2003년도 ISIS 2003
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    • pp.66-69
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    • 2003
  • This paper considers a reinforcement learning(RL) which deals with real environments. Most reinforcement learning studies have been made by simulations because real-environment learning requires large computational cost and much time. Furthermore, it is more difficult to acquire many rewards efficiently in real environments than in virtual ones. The most important requirement to make real-environment learning successful is the appropriate construction of the state space. In this paper, to begin with, I show the basic overview of the reinforcement learning under real environments. Next, 1 introduce a state-space construction method under real environmental which is State Partition Method. Finally I apply this method to a robot navigation problem and compare it with conventional methods.

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Static response of 2-D functionally graded circular plate with gradient thickness and elastic foundations to compound loads

  • Behravan Rad, A.
    • Structural Engineering and Mechanics
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    • 제44권2호
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    • pp.139-161
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    • 2012
  • In this paper, the static behavior of bi-directional functionally graded (FG) non-uniform thickness circular plate resting on quadratically gradient elastic foundations (Winkler-Pasternak type) subjected to axisymmetric transverse and in-plane shear loads is carried out by using state-space and differential quadrature methods. The governing state equations are derived based on 3D theory of elasticity, and assuming the material properties of the plate except the Poisson's ratio varies continuously throughout the thickness and radius directions in accordance with the exponential and power law distributions. The stresses and displacements distribution are obtained by solving state equations. The effects of foundation stiffnesses, material heterogeneity indices, geometric parameters and loads ratio on the deformation and stress distributions of the FG circular plate are investigated in numerical examples. The results are reported for the first time and the new results can be used as a benchmark solution for future researches.

Modeling and Simulation Technique of Two Quadrant Chopper and PWM Inverter-Fed IPMSM Drive System and Its Application to Hybrid Vehicles

  • Murata, Toshiaki;Kawatsu, Utaro;Tamura, Junji;Tsuchiya, Takeshi
    • Journal of international Conference on Electrical Machines and Systems
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    • 제1권2호
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    • pp.91-97
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    • 2012
  • This paper presents a state space model of a two quadrant chopper and PWM inverter-fed Interior Permanent Magnet Synchronous Motor (IPMSM) drive system and its application to hybrid vehicles. The drive system has two different state equations for motoring and regenerating action. This paper presents a common state equation by using State Space Averaging method. Using this model of the IPMSM drive system, detailed simulation and controller design of the drive system, including PWM inverter switching, are given. The validity of this model and usefulness, according to a comparison among Maximum Torque/Ampere control, Maximum Torque/Flux control, and Maximum Efficiency optimization, are confirmed from simulation results.