<![CDATA[ IEEE Transactions on Aerospace and Electronic Systems - new TOC ]]>
http://ieeexplore.ieee.org
TOC Alert for Publication# 7 2017February 16<![CDATA[IEEE Aerospace and Electronic Systems Society [Front inside cover]]]>526c1c2106<![CDATA[IEEE Aerospace and Electronic Systems Society [Front inside cover]]]>526c3c383<![CDATA[Information for Authors]]>526ii41<![CDATA[From the Editor-in-Chief]]>52626112611173<![CDATA[Robust SAR STAP via Kronecker decomposition]]>526261226251470<![CDATA[Multistatic Bayesian extended target tracking]]>526262626431610<![CDATA[Topological and statistical behavior classifiers for tracking applications]]>526264426612962<![CDATA[3D automatic target recognition for future LIDAR missiles]]>526266226752137<![CDATA[Symmetrical difference pattern monopulse for low-angle tracking with array radar]]>52626762684815<![CDATA[An integrated tailoring model for thermal cycling tests of spacecraft electronics]]>526268526962709<![CDATA[Multifeature-based importance weighting for the PHD SLAM filter]]>526269727144691<![CDATA[Focusing highly squinted Azimuth variant Bistatic SAR]]>526271527302071<![CDATA[Chernoff fusion of Gaussian mixtures based on sigma-point approximation]]>52627322746900<![CDATA[Orbiter-to-orbiter tomography: a potential approach for small solar system bodies]]>526274727598882<![CDATA[Game theoretic analysis for MIMO radars with multiple targets]]>526276027741888<![CDATA[A mixed L<sub>2</sub>/Lα differential game approach to pursuit-evasion guidance]]>2/Lα guidance law, is derived for a missile with large lateral acceleration capability intercepting an evading target that has limited lateral acceleration capability. The engagement is formulated as a two-person zero-sum pursuit-evasion game with a linear quadratic cost, where only the maneuverability of the evader is assumed bounded. The open-loop solution is derived via direct derivation of the lower and upper values of the game and the saddle point condition. It is shown that the existence of an open-loop saddle point solution depends on the initial conditions of the engagement. A closed-form guidance law is formulated, consisting of the optimal saddle point strategies and three proposed variants when no saddle point solution exists. Linear and nonlinear simulations are performed for the case of a pursuer with first-order control dynamics and an evader with zero-lag dynamics in order to illustrate the advantages and performance of the proposed guidance algorithm in comparison with classical optimal and differential game–based guidance laws.]]>526277527881875<![CDATA[Radar imaging of micromotion targets from corrupted data]]>526278928021332<![CDATA[Fast coherent integration for maneuvering target with high-order range migration via TRT-SKT-LVD]]>526280328141728<![CDATA[Fast corrections for polar format algorithm with a curved flight path]]>526281528242123<![CDATA[Sum and difference beamforming for angle-doppler estimation with STAP-based radars]]>526282528372114<![CDATA[Processing video-SAR data with the fast backprojection method]]>2 log N) complexity through a recursive procedure. To reduce the processing complexity in video-SAR system, the scene is partitioned into the general region (GR) and the region of interest (ROI). In different regions, different aperture lengths are used. The proposed method allows a direct trade between processing speed and focused quality for the GR, meanwhile reserving particular details in the ROI. The effectiveness is validated both for a simulated scene and for X-band SAR measurements from the Gotcha data set.]]>526283828481628<![CDATA[Large scale image aided navigation]]>52628492860589<![CDATA[SAR ATR by a combination of convolutional neural network and support vector machines]]>526286128722067<![CDATA[Private proximity detection using partial GPS information]]>5262873288516860<![CDATA[Myths concerning Woodward's ambiguity function: analysis and resolution]]>52628862895797<![CDATA[Optical beam position estimation in free-space optical communication]]>52628962905962<![CDATA[A fast load-pull optimization for power-added efficiency under output power and ACPR constraints]]>526290629163159<![CDATA[100-Mb/s enhanced data rate MIL-STD-1553B controller in 65-nm CMOS technology]]>2 for a target bit error rate (BER) of 10^{-7}.]]>526291729294836<![CDATA[Inverse problems-based maximum likelihood estimation of ground reflectivity for selected regions of interest from stripmap SAR data]]>526293029391242<![CDATA[Star identification based on euclidean distance transform, voronoi tessellation, and k-nearest neighbor classification]]>526294029492107<![CDATA[Efficient ISAR autofocus via minimization of Tsallis Entropy]]>526295029601558<![CDATA[Cramer-Rao lower bound for round-trip delay ranging with subcarrier-interleaved OFDMA]]>526296129721225<![CDATA[Tracking of extended object or target group using random matrix: new model and approach]]>526297329891381<![CDATA[Level-set random hypersurface models for tracking nonconvex extended objects]]>526299030072180<![CDATA[Quad-segment polynomial trajectory guidance for impact-time control of precision-munition strike]]>526300830232485<![CDATA[Horizontal-vertical guidance of Quadrotor for obstacle shape mapping]]>526302430352917<![CDATA[Distributed TLS over multitask networks with adaptive intertask cooperation]]>526303630521171<![CDATA[Focused energy delivery with protection for precision electronic warfare]]>526305330641501<![CDATA[Nonsparsity influence on the ISAR recovery from reduced data [Correspondence]]]>52630653070424<![CDATA[Improved FH acquisition scheme in partial-band noise jamming [Correspondence]]]>52630703076775<![CDATA[Coverage and rate analysis of aerial base stations [Letter]]]>52630773081777<![CDATA[Technical areas & editors: Aerospace and Electronic Systems Society]]>52630823088300