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TOC Alert for Publication# 7 2014December 18<![CDATA[Table of Contents]]>504c1c4149<![CDATA[IEEE Aerospace and Electronic Systems Society [Front inside cover]]]>504c2c2101<![CDATA[Information for authors]]>504c3c352<![CDATA[How are we doing? October 2014]]>504241524161301<![CDATA[Singular perturbationlike approach to compensation of actuator dynamics effect in missile control]]>504241724392251<![CDATA[Demonstration of cognitive radar for target localization under interference]]>504244024552497<![CDATA[Analysis of code phase estimation error from resolved first arrival path]]>50424562467665<![CDATA[Full- and reduced-order distributed Bayesian estimation analytical performance bounds]]>504246824881050<![CDATA[Adaptive single-frame superresolution for detecting closely spaced IR targets in clutter]]>504248924995512<![CDATA[Extreme-value analysis for ML-PMHT, Part 1: threshold determination]]>504250025141143<![CDATA[Extreme-value analysis for mlML-PMHT, Part 2: target trackability]]>504251525271806<![CDATA[Efficient target detection using an adaptive compressive imager]]>504252825401296<![CDATA[Direction finding algorithms based on joint iterative subspace optimization]]>504254125531399<![CDATA[A low complexity parameter estimation technique for LFMCW signals]]>504255425631022<![CDATA[Adaptive beamforming for low-angle target tracking under multipath interference]]>504256425772656<![CDATA[Feedback control for spacecraft reorientation under attitude constraints via convex potentials]]>504257825921921<![CDATA[Performance prediction of feature-aided track-to-track association]]>504259326031029<![CDATA[MIMO adaptive beamforming for nonseparable multipath clutter mitigation]]>504260426182119<![CDATA[IM-filter for INS/GPS-integrated navigation system containing low-cost gyros]]>504261926291222<![CDATA[Improved reliability-based decision support methodology applicable in system-level failure diagnosis and prognosis]]>50426302641910<![CDATA[Modal estimation by FBG for flexible structures attitude control]]>504264226532159<![CDATA[GPS-based attitude determination for a spinning rocket]]>504265426633351<![CDATA[Sensor selection for nonlinear systems in large sensor networks]]>50426642678724<![CDATA[Bias analysis of maximum likelihood target location estimator]]>50426792693904<![CDATA[Target tracking in a collaborative sensor network]]>504269427141959<![CDATA[Aerial-terrestrial communications: terrestrial cooperation and energy-efficient transmissions to aerial base stations]]>504271527352726<![CDATA[Algorithms for accurate LEO geomagnetic measurements with satellite-mounted magnetometers]]>504273627451229<![CDATA[Prediction and retrodiction algorithms for path-constrained targets]]>504274627611406<![CDATA[Radar code design for detection of moving targets]]>504276227781826<![CDATA[Integrity monitoring with vector GNSS receivers]]>504277927931588<![CDATA[New decision variables for GNSS acquisition in the presence of CW interference]]>504279428061499<![CDATA[Verification of a CubeSat via hardware-in-the-loop simulation]]>504280728181523<![CDATA[Condition monitoring of helicopter drive shafts using quadratic-nonlinearity metric based on cross-bispectrum]]>504281928292112<![CDATA[Spaceborne SIMO-SAR for three-dimensional ionospheric irregularity sounding]]>504283028465574<![CDATA[Formation flying with nonlinear partial integrated guidance and control]]>504284728593169<![CDATA[Distributed ionosphere monitoring by collaborating mobile receivers]]>50428602869571<![CDATA[New chirp sequence radar waveform]]>r simultaneously and unambiguously with high accuracy and resolution even in multitarget situations, which is a matter of the appropriate waveform design. Based on a single continuous wave chirp transmit signal, target range R and radial velocity v_{r} cannot be measured in an unambiguous way. Therefore a so-called multiple frequency shift keying (MFSK) transmit signal was developed, which is applied to measure target range and radial velocity separately and simultaneously. In this case the radar measurement is based on a frequency and additionally on a phase measurement, which suffers from a lower estimation accuracy compared with a pure frequency measurement. This MFSK waveform can therefore be improved and outperformed by a chirp sequences waveform. Each chirp signal has in this case very short time duration T_{chirp}. Therefore the measured beat frequency f_{B} is dominated by target range R and is less influenced by the radial velocity v_{r}. The range and radial velocity estimation is based on two separate frequency measurements with high accuracy in both cases. Classical chirp sequence waveforms suffer from possible ambiguities in the velocity measurement. It is the objective of this paper to modify the classical chirp sequence to get an unambiguous velocity measurement even in multitarget situations.]]>504287028771017<![CDATA[Distributed computation for direct position determination emitter location]]>504287828892032<![CDATA[Pylon line spatial correlation assisted transmission line detection]]>504289029054166<![CDATA[Differential games missile guidance with bearings-only measurements]]>504290629151398<![CDATA[Modeling cratered surfaces with real and synthetic terrain for testing planetary landers]]>504291629281875<![CDATA[Near-far interference mitigation for pseudolites using double transmission]]>50429292941426<![CDATA[Approximate evaluation of marginal association probabilities with belief propagation]]>504294229591794<![CDATA[PMHT with timing uncertainty]]>50429602973928<![CDATA[Bearings-only constant velocity target maneuver detection via expected likelihood]]>504297429881284<![CDATA[Adaptive moving target indication in a windblown clutter environment]]>504298929971686<![CDATA[Investigation on an ultra–wide-swath, multiple-elevation-beam SAR based on sweep-PRI mode]]>504299830203866<![CDATA[Modeling of extended objects based on support functions and extended Gaussian images for target tracking]]>504302130351743<![CDATA[Relative pose estimation for cylinder-shaped spacecrafts using single image]]>504303630563643<![CDATA[Subarray-based frequency diverse array radar for target range-angle estimation]]>504305730671429<![CDATA[Random set theoretic soft/hard data fusion framework]]>50430683081785<![CDATA[Robust H<sub>∞</sub> autopilot design for agile missile with time-varying parameters]]>∞ loop shaping for an agile missile that experiences high angle of attack, highly nonlinear and rapidly changing dynamics, and aerodynamic variation after launch. The main autopilot design is started with two H_{∞} control designs intended to cover the low-speed and high-speed regions of the flight envelope. Then, the two control designs are combined (via Mach variation) to construct a global controller that covers the entire flight envelope. The proposed autopilots have a simple structure and require no time-consuming gain scheduling for many flight conditions, while providing satisfactory tracking and robustness over the entire flight envelope. The performance of the designed autopilots is checked via a comparison study and a challenging intercept scenario. These performance test results clearly demonstrate the merit of the proposed designs.]]>504308230891572<![CDATA[Augmented L<sub>1</sub> adaptive tracking control of quad-rotor unmanned aircrafts]]>1 adaptive control methodology augmented with nonlinear feed-forward compensations. The proposed augmented L_{1} adaptive controller achieves uniformly bounded transient and asymptotic tracking of the output signal for any designated bounded reference trajectory. Finally, simulations of tracking a circular reference trajectory are performed to illustrate the validity of the proposed controller.]]>504309031013028<![CDATA[3D interferometric ISAR imaging of noncooperative targets]]>504310231141979<![CDATA[Unified turbo/LDPC code decoder architecture for deep-space communications]]>2) and very low power consumption (2.1 mW).]]>50431153125675<![CDATA[In-orbit estimation of time-varying residual magnetic moment]]>50431263136570<![CDATA[Detection performance of spatial-frequency diversity MIMO radar]]>504313731552694<![CDATA[Expectation maximization-based detection in range-heterogeneous weibull clutter]]>504315631662402<![CDATA[Active power management system for an unmanned aerial vehicle powered by solar cells, a fuel cell, and batteries]]>504316731772717<![CDATA[Three-dimensional target motion analysis using azimuth/elevation angles]]>50431783194667<![CDATA[Decoupled ISAR imaging using RSFW based on twice compressed sensing]]>504319532112806<![CDATA[Combined GPS L1C/A and L2C signal acquisition architectures leveraging differential combination]]>5043212322911691<![CDATA[Carrier phase null space monitor for ionospheric gradient detection]]>50432303243878<![CDATA[Guidance for scatter-regather maneuvers of disaggregated satellites]]>2-perturbed nonlinear dynamical model through a backstepping approach. Numerical simulations that include the effects of the zonal harmonics J_{2} to J_{5} are used to demonstrate the effectiveness of the proposed guidance law.]]>50432353243409<![CDATA[Editors for Technical Fields of Interest]]>504324632504594