无人飞行器航迹规划方法综述

首先从不同角度给出航迹规划的两种定义,把航迹规划问题拆分为规划空间、航迹表示、约束条件、目标函数、规划算法五个子问题,提出了适用于各类无人飞行器航迹规划问题分析求解的过程模型。对规划空间构造方法、目标函数、规划算法进行分类比较,并给出每种方法的优、缺点及适用范围,辅助规划人员针对具体需求快速明确规划思路并选择算法。最后指出了航迹规划未来面临的新问题、新挑战。     

Neural control of smart electromagnetic structures [patch antennas]

Smart electromagnetic structures (SEMS) are capable of interacting with the surrounding electromagnetic field and responding to it. A system is “smart” when it integrates sensing, processing, and control elements (e.g. antennas, neural networks, diodes) in an autonomous manner. A SEMS capable of tuning frequency autonomously is described. Data are presented showing that the system can extend the useable bandwidth of a microstrip patch antenna in a frequency hop environment to more than twice the static value     

A review of uncertainty in flight vehicle structural damage monitoring,diagnosis and control: Challenges and opportunities

This paper presents a comprehensive review of uncertainties involved in flight vehicle structural damage monitoring, diagnosis, prognosis and control. Uncertainties can cause infeasibilities, false diagnosis and very imprecise prognosis if not correctly taken into account. The purpose of this paper is to review existing methods that have been developed to address the problem of uncertainty in the area of damage sensing, diagnosis, prognosis and control in flight vehicles. The mathematical and statistical methods in analyzing uncertainty are first presented and compared. Then, the different sources and perspectives of uncertainties in the damage assessment process are presented and classified. Following this, diagnosis and prognosis methods are reviewed. Final review section covers the control of damaged structure under uncertainty. In each section and in the concluding remarks section the research challenges in the field of flight vehicle structural damage sensing, diagnosis and prognosis methods as well as control under uncertainty are identified and promising new ideas are discussed.     

Stability and control [A century of powered flight 1903-2003]

Aircraft stability and control has evolved from stick and rudder through stability augmentation to redundant digital flight control systems (FCS) and finally to digital fly-by-wire (FBW). Substantial advances in avionics have occurred as aviation progressed from biplanes to civil transports to sub/supersonic military craft and finally the Space Shuttle. Aircraft stability can be defined as aircraft control by maintaining a favorable relationship between center of gravity (CG) and the center of pressure (CP).     

自适应二阶动态terminal滑模在近空间飞行器控制中的应用

为克服滑模抖振,设计了二阶动态terminal滑模,得到在时间本质上连续的控制器,并使滑模面在有限时间内收敛.然后采用非线性干扰观测器逼近复合干扰,通过在控制器中设置自适应补偿项,放宽了非线性干扰观测器的假设条件,不再要求复合干扰变化率为零.基于李雅普诺夫理论,严格证明了系统稳定性.最后将提出的控制方案应用于近空间飞行器姿态角跟踪仿真实验,仿真结果表明了该控制方案的有效性及优越性.      

Overview of some optimal control methods adapted to expendable and reusable launch vehicle trajectories

Launcher trajectory optimization is a complex task, especially when considering the specific problems arising in the study of reusable launch vehicles. Part of the difficulty comes from the different characteristics of the trajectory arcs which make up the vehicle's mission (constraints and controls may not be the same). Another difficulty is the necessity, in some cases, of a global optimization between ascent and re-entry phases (branching optimisation). Finally, optimization tools devoted to this task should be polyvalent and robust, as the studies of reusable launch vehicles usually cover many different concepts, and also many different trajectory cases (such as abort scenarios). The purpose of this paper is to present different approaches used in France by CNES and ONERA to solve optimal control problems in the context of launcher trajectory optimization. These approaches, which are powerful implementations of classical optimization methods, were designed to cover the needs for both expendable and reusable launchers trajectory calculation. The first optimization tool presented is OPTAX, which uses an indirect shooting method. The second and third tools presented are CNES's ORAGE and ONERA's FLOP/OLGA, which use two different variants of the gradient method. The paper describes the equations and methodology behind these tools, and also presents their advantages and drawbacks.     

System sensitivity to parametric variations in the problem of lateral motion flight vehicle control

The results of investigation of dynamic system sensitivity to parametric variations in the channel of flight vehicle lateral motion are presented using the notion of infinitesimal transformation. The exact relationships establishing a link between the structure of parameter deviation and that of system phase coordinate deviation are obtained.     

Teaching old tricks to new dogs [automatic test equipment]

This describes why transferring test programs and fixtures from obsolete automatic test equipment (ATE) to new equipment are not as simple as it should be. No one would argue that technology has made major advances on test in the last 30 years. Today, speed, overall performance, computing power, and software tools are more sophisticated than 20 or 30 years ago, when the first ATE appeared. As these ATE now head for retirement and as the programs they support still have a long life to live, one would think legacy replacement with new ATE would be a simple task. Unfortunately, this is seldom the case. We realize that old ATE had a number of cards up their sleeves to deal with. For example, high voltage technology, lack of computer aided engineering (CAE) data, requirements for parametric tests, extensive usage of the guided probe, and many other aspects might be not so simple to be reproduced with modern, yet powerful, ATE. The paper shall identify the specific constraints involved with old technology and give examples of success stories where new ATE has been adapted to respond to the challenge. Paraphrasing (in reverse) and old saying, it is like "teaching old tricks to new dogs".     

Real-time expert systems for advanced power control (a statusupdate) [aerospace power system testbed]

The most recent developments in the Boeing Aerospace Autonomous Power System (APS) testbed are presented. The APS testbed is a 28-VDC system with 3-kW capability, assembled for use in developing improved control, techniques for aerospace electrical power systems. The main emphasis is on the development of a sophisticated programming environment to control concurrent execution of multiple autonomous algorithms coupled with a continuous input/output data flow. The integration of high-level control algorithms used for battery charge control into a real-time execution environment is discussed. This includes methods that allow several functions to respond to real-time input, affect/maintain expert system (shared) memory, and control the electrical power system configuration. Sophisticated schemes for scheduling these expert system control functions are required to allow real-time multitasking     

Communications Award to Robert D. Briskman [Society News & Information]

The American Institute of Aeronautics and Astronautics presented Robert D. Briskman with the Aerospace Communications Award at their 25th International Communications Satellite Systems Conference, in Seoul, Korea, on April 12, 2007.     

On the resolvability of sinusoidal parameter estimates [andapplication to SAR target features]

The resolvability of 2-D (two-dimensional) sinusoidal parameter estimates is studied. These sinusoids describe the target features in SAR (synthetic aperture radar) applications. We analyze the resolvability by considering the frequency estimates of the sinusoids. Our results may be used by target classification algorithms to better classify radar targets in SAR applications     

Functional analysis: a system conceptual design tool [andapplication to ATC system]

Functional analysis is a methodology for analyzing the mission and performance requirements of a system, and translating them into discrete activities or tasks which must be performed by the system. Determination of the system's functionality is the first step in obtaining a conceptual view of a system that is to be designed. The methodology for conducting functional analysis is developed, some of the tools used to support the activity are described, including examples to help solidify the concepts presented     

Multiassignment for tracking a large number of overlapping objects[and application to fibroblast cells]

In this paper we present a new technique for data association using multiassignment for tracking a large number of closely spaced (and overlapping) objects. The algorithm is illustrated on a biomedical problem, namely the tracking of a group of fibroblast (tissue) cells from an image sequence, which motivated this work. Because of their proximity to one another and due to the difficulties in segmenting the images accurately from a poor-quality image sequence, the cells are effectively closely spaced objects (CSOs). The algorithm presents a novel dichotomous, iterated approach to multiassignment using successive one-to-one assignments of decreasing size with modified costs. The cost functions, which are adjusted depending on the “depth” of the current assignment level and on the tracking results, are derived. The resulting assignments are used to form, maintain and terminate tracks with a modified version of the probabilistic data association (PDA) filter, which can handle the contention for a single measurement among multiple tracks in addition to the association of multiple measurements to a single track. Estimation results are given and compared with those of the standard 2D one-to-one assignment algorithm. It is shown that iterated multiassignment results in superior measurement-to-track association. The algorithms presented can be used for other general tracking problems, including dense air traffic surveillance and control     

Observability analysis of piece-wise constant systems. II.Application to inertial navigation in-flight alignment [militaryapplications]

For pt.I see ibid., vol.28, no.4, p.1056-67, Oct. 1992. The method of analyzing the observability of time-varying linear systems as piecewise constant systems (PWCS) is applied to the analysis of in-flight alignment (IFA) of inertial navigation systems (INS) whose estimability is known to be enhanced by maneuvers. The validity of this approach to the analysis of IFA is proven. The analysis lays the theoretical background to, and clearly demonstrates the observability enhancement of, IFA. The analytic conclusions are confirmed by covariance simulations. Although INS IFA was handled to various degrees in the past, a comprehensive control theoretic approach to the problem is introduced. The analysis yields practical conclusions and a procedure previously unknown