相关期刊:《东南大学学报(自然科学版)》《Computers, Materials & Continua》《Journal of Beijing Institute of Technology》《Transactions of Nanjing University of Aeronautics and Astronautics》更多>>
In this paper,an integrated estimation guidance and control(IEGC)system is designed based on the command filtered backstepping approach for circular field-of-view(FOV)strapdown missiles.The threedimensional integrated...
sponsored by the National Natural Science Foundation of China under Grant No.51979275;the Joint Open Research Fund Program of State Key Laboratory of Hydroscience and Engineering and Tsinghua—Ningxia Yinchuan Joint Institute of Internet of Waters on Digital Water Governance under Grant No.sklhse-2022-Iow08;the Open Fund of Key Laboratory of Urban Land Resources Monitoring and Simulation,Ministry of Natural Resources under Grant No.KF-2021-06-115;the National Key R&D Program of China under Grant No.2018YFD0700603;the 2115 Talent Development Program of China Agricultural University.
Aiming at intercepting large maneuvering targets precisely,the guidance law of advanced self-seeking missiles requires not only inertial line-of-sight(LOS)angular rate but also target maneuvering acceleration.Moreover...
This work is funded by Natural Science Foundation of Jiangsu Province under Grant BK20160955;a project funded by the Priority Academic Program Development of Jiangsu Higher Education Institutions and Science Research Foundation of Nanjing University of Information Science and Technology under Grant 20110430;Open Foundation of Jiangsu Key Laboratory of Meteorological Observation and Information Processing(KDXS1304);Open Foundation of Jiangsu Key Laboratory of Ocean Dynamic Remote Sensing and Acoustics(KHYS1405)。
Strapdown non-exchangeable error compensation technology in high dynamic environment is one of the key technologies of strapdown inertial navigation system.Mathematical platform is used in strapdown inertial navigatio...
supported by the National Natural Science Foundation of China(61722301)
Strapdown inertial navigation system(SINS)/celestial navigation system(CNS)integrated navigation is widely used to achieve long-time and high-precision autonomous navigation for aircraft.In general,SINS/CNS integrated...
supported by the Armament Research Fund of China (No.9020A02010313BQ01)
This paper focuses mainly on semi-strapdown image homing guided (SSIHG) system design based on optical flow for a six-degree-of-freedom (6-DOF) axial-symmetric skid-to-turn missile. Three optical flow algorithms s...
supported by the National Natural Science Foundation of China(No.61375082)
The state estimation strategy using the smooth variable structure filter (SVSF) is based on the variable structure and sliding mode concepts. As presented in its standard form with a fixed boundary layer limit, the ...
Supported by the National Natural Science Foundation of China(61104188,91016019);the National Basic Research Program of China(2009CB724002);the Research Funding of Nanjing University of Aeronautics and Astronautics(NS2010084,NP2011049)
Traditional coning algorithms are based on the first-order coning correction reference model.Usually they reduce the algorithm error of coning axis(z)by increasing the sample numbers in one iteration interval.But the ...
supported by the Astronautical Support Foundation of China (2009HTXGD)
The precision of the laser gyro used in tactical missiles is poor because of dithering frequency,actuating by vibration,shock and overload in dynamical environment.This paper introduces the transfer matrix method of t...
The rigid body motion can be represented by a motor in geometric algebra, and the motor can be rewritten as a trinometric function of the screw blade. In this paper, a screw blade strapdown inertial navigation system ...