Advanced Trajectory Optimization, Guidance and Control Strategies for Aerospace Vehicles

Advanced Trajectory Optimization, Guidance and Control Strategies for Aerospace Vehicles
Author: Runqi Chai
Publisher: Springer Nature
Total Pages: 272
Release: 2023-10-29
Genre: Technology & Engineering
ISBN: 9819943116

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This book focuses on the design and application of advanced trajectory optimization and guidance and control (G&C) techniques for aerospace vehicles. Part I of the book focuses on the introduction of constrained aerospace vehicle trajectory optimization problems, with particular emphasis on the design of high-fidelity trajectory optimization methods, heuristic optimization-based strategies, and fast convexification-based algorithms. In Part II, various optimization theory/artificial intelligence (AI)-based methods are constructed and presented, including dynamic programming-based methods, model predictive control-based methods, and deep neural network-based algorithms. Key aspects of the application of these approaches, such as their main advantages and inherent challenges, are detailed and discussed. Some practical implementation considerations are then summarized, together with a number of future research topics. The comprehensive and systematic treatment of practical issues in aerospace trajectory optimization and guidance and control problems is one of the main features of the book, which is particularly suitable for readers interested in learning practical solutions in aerospace trajectory optimization and guidance and control. The book is useful to researchers, engineers, and graduate students in the fields of G&C systems, engineering optimization, applied optimal control theory, etc.

Design of Trajectory Optimization Approach for Space Maneuver Vehicle Skip Entry Problems

Design of Trajectory Optimization Approach for Space Maneuver Vehicle Skip Entry Problems
Author: Runqi Chai
Publisher: Springer
Total Pages: 207
Release: 2019-07-30
Genre: Technology & Engineering
ISBN: 9811398453

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This book explores the design of optimal trajectories for space maneuver vehicles (SMVs) using optimal control-based techniques. It begins with a comprehensive introduction to and overview of three main approaches to trajectory optimization, and subsequently focuses on the design of a novel hybrid optimization strategy that combines an initial guess generator with an improved gradient-based inner optimizer. Further, it highlights the development of multi-objective spacecraft trajectory optimization problems, with a particular focus on multi-objective transcription methods and multi-objective evolutionary algorithms. In its final sections, the book studies spacecraft flight scenarios with noise-perturbed dynamics and probabilistic constraints, and designs and validates new chance-constrained optimal control frameworks. The comprehensive and systematic treatment of practical issues in spacecraft trajectory optimization is one of the book’s major features, making it particularly suited for readers who are seeking practical solutions in spacecraft trajectory optimization. It offers a valuable asset for researchers, engineers, and graduate students in GNC systems, engineering optimization, applied optimal control theory, etc.

Guidance and Control Strategies for Aerospace Vehicles

Guidance and Control Strategies for Aerospace Vehicles
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
Total Pages: 100
Release: 2018-07-08
Genre:
ISBN: 9781722425449

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A neighboring optimal guidance scheme was devised for a nonlinear dynamic system with stochastic inputs and perfect measurements as applicable to fuel optimal control of an aeroassisted orbital transfer vehicle. For the deterministic nonlinear dynamic system describing the atmospheric maneuver, a nominal trajectory was determined. Then, a neighboring, optimal guidance scheme was obtained for open loop and closed loop control configurations. Taking modelling uncertainties into account, a linear, stochastic, neighboring optimal guidance scheme was devised. Finally, the optimal trajectory was approximated as the sum of the deterministic nominal trajectory and the stochastic neighboring optimal solution. Numerical results are presented for a typical vehicle. A fuel-optimal control problem in aeroassisted noncoplanar orbital transfer is also addressed. The equations of motion for the atmospheric maneuver are nonlinear and the optimal (nominal) trajectory and control are obtained. In order to follow the nominal trajectory under actual conditions, a neighboring optimum guidance scheme is designed using linear quadratic regulator theory for onboard real-time implementation. One of the state variables is used as the independent variable in reference to the time. The weighting matrices in the performance index are chosen by a combination of a heuristic method and an optimal modal approach. The necessary feedback control law is obtained in order to minimize the deviations from the nominal conditions. Hibey, J. L. and Naidu, D. S. and Charalambous, C. D. Unspecified Center...

Advanced Control of Aircraft, Spacecraft and Rockets

Advanced Control of Aircraft, Spacecraft and Rockets
Author: Ashish Tewari
Publisher: John Wiley & Sons
Total Pages: 416
Release: 2011-06-01
Genre: Technology & Engineering
ISBN: 1119972744

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Advanced Control of Aircraft, Spacecraft and Rockets introduces the reader to the concepts of modern control theory applied to the design and analysis of general flight control systems in a concise and mathematically rigorous style. It presents a comprehensive treatment of both atmospheric and space flight control systems including aircraft, rockets (missiles and launch vehicles), entry vehicles and spacecraft (both orbital and attitude control). The broad coverage of topics emphasizes the synergies among the various flight control systems and attempts to show their evolution from the same set of physical principles as well as their design and analysis by similar mathematical tools. In addition, this book presents state-of-art control system design methods - including multivariable, optimal, robust, digital and nonlinear strategies - as applied to modern flight control systems. Advanced Control of Aircraft, Spacecraft and Rockets features worked examples and problems at the end of each chapter as well as a number of MATLAB / Simulink examples housed on an accompanying website at http://home.iitk.ac.in/~ashtew that are realistic and representative of the state-of-the-art in flight control.

Autonomous Trajectory Planning and Guidance Control for Launch Vehicles

Autonomous Trajectory Planning and Guidance Control for Launch Vehicles
Author: Zhengyu Song
Publisher: Springer Nature
Total Pages: 229
Release: 2023-04-15
Genre: Science
ISBN: 981990613X

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This open access book highlights the autonomous and intelligent flight control of future launch vehicles for improving flight autonomy to plan ascent and descent trajectories onboard, and autonomously handle unexpected events or failures during the flight. Since the beginning of the twenty-first century, space launch activities worldwide have grown vigorously. Meanwhile, commercial launches also account for the booming trend. Unfortunately, the risk of space launches still exists and is gradually increasing in line with the rapidly rising launch activities and commercial rockets. In the history of space launches, propulsion and control systems are the two main contributors to launch failures. With the development of information technologies, the increase of the functional density of hardware products, the application of redundant or fault-tolerant solutions, and the improvement of the testability of avionics, the launch losses caused by control systems exhibit a downward trend, and the failures induced by propulsion systems become the focus of attention. Under these failures, the autonomous planning and guidance control may save the missions. This book focuses on the latest progress of relevant projects and academic studies of autonomous guidance, especially on some advanced methods which can be potentially real-time implemented in the future control system of launch vehicles. In Chapter 1, the prospect and technical challenges are summarized by reviewing the development of launch vehicles. Chapters 2 to 4 mainly focus on the flight in the ascent phase, in which the autonomous guidance is mainly reflected in the online planning. Chapters 5 and 6 mainly discuss the powered descent guidance technologies. Finally, since aerodynamic uncertainties exert a significant impact on the performance of the ascent / landing guidance control systems, the estimation of aerodynamic parameters, which are helpful to improve flight autonomy, is discussed in Chapter 7. The book serves as a valuable reference for researchers and engineers working on launch vehicles. It is also a timely source of information for graduate students interested in the subject.

Computational Guidance and Control for Aerospace Systems

Computational Guidance and Control for Aerospace Systems
Author: Taylor Patrick Reynolds
Publisher:
Total Pages: 258
Release: 2020
Genre:
ISBN:

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The objective of this dissertation is to develop new techniques that advance the state of the art in optimization-based trajectory generation. Two complementary techniques are studied. First, explicit trajectory generation computes a single path that connects two boundary conditions. For a general optimal control problem, sequential convex programming is used to design iterative algorithms that solve challenging aerospace problems. The limited power available on a spacecraft has long been at odds with the computationally demanding algorithms required to solve such problems, and so specialized techniques for developing real-time capable implementations of these algorithms are presented. Runtime analysis offers initial evidence that it is possible to solve explicit trajectory optimization problems reliably and fast enough to be considered a viable technology. As an alternative approach, implicit trajectory generation computes a set of functions that implicitly define an entire set of trajectories. By carrying out more extensive offline computations, it is shown that a feasible trajectory can be obtained from a wide array of initial conditions by using numerical integration. Consequently, the required real-time computations are significantly reduced compared to explicit trajectory optimization algorithms. Implicit trajectory generation methods can also offer a stronger theoretical, and offline-certifiable, guarantee that a feasible trajectory will be available for a prescribed set of vehicle conditions. Examples in powered descent and satellite attitude control are used to demonstrate each method.

Spacecraft Trajectory Optimization

Spacecraft Trajectory Optimization
Author: Bruce A. Conway
Publisher: Cambridge University Press
Total Pages: 313
Release: 2010-08-23
Genre: Technology & Engineering
ISBN: 113949077X

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This is a long-overdue volume dedicated to space trajectory optimization. Interest in the subject has grown, as space missions of increasing levels of sophistication, complexity, and scientific return - hardly imaginable in the 1960s - have been designed and flown. Although the basic tools of optimization theory remain an accepted canon, there has been a revolution in the manner in which they are applied and in the development of numerical optimization. This volume purposely includes a variety of both analytical and numerical approaches to trajectory optimization. The choice of authors has been guided by the editor's intention to assemble the most expert and active researchers in the various specialities presented. The authors were given considerable freedom to choose their subjects, and although this may yield a somewhat eclectic volume, it also yields chapters written with palpable enthusiasm and relevance to contemporary problems.

Analytical Investigations in Aircraft and Spacecraft Trajectory Optimization and Optimal Guidance

Analytical Investigations in Aircraft and Spacecraft Trajectory Optimization and Optimal Guidance
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
Total Pages: 188
Release: 2018-07-17
Genre:
ISBN: 9781722945305

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A collection of analytical studies is presented related to unconstrained and constrained aircraft (a/c) energy-state modeling and to spacecraft (s/c) motion under continuous thrust. With regard to a/c unconstrained energy-state modeling, the physical origin of the singular perturbation parameter that accounts for the observed 2-time-scale behavior of a/c during energy climbs is identified and explained. With regard to the constrained energy-state modeling, optimal control problems are studied involving active state-variable inequality constraints. Departing from the practical deficiencies of the control programs for such problems that result from the traditional formulations, a complete reformulation is proposed for these problems which, in contrast to the old formulation, will presumably lead to practically useful controllers that can track an inequality constraint boundary asymptotically, and even in the presence of 2-sided perturbations about it. Finally, with regard to s/c motion under continuous thrust, a thrust program is proposed for which the equations of 2-dimensional motion of a space vehicle in orbit, viewed as a point mass, afford an exact analytic solution. The thrust program arises under the assumption of tangential thrust from the costate system corresponding to minimum-fuel, power-limited, coplanar transfers between two arbitrary conics. The thrust program can be used not only with power-limited propulsion systems, but also with any propulsion system capable of generating continuous thrust of controllable magnitude, and, for propulsion types and classes of transfers for which it is sufficiently optimal the results of this report suggest a method of maneuvering during planetocentric or heliocentric orbital operations, requiring a minimum amount of computation; thus uniquely suitable for real-time feedback guidance implementations. Markopoulos, Nikos and Calise, Anthony J. Unspecified Center AIRCRAFT GUIDANCE; CONTROLLERS; FLIGHT PATHS; OPTIMAL CONTROL...

Trajectory Optimization and Guidance Law Development for National Aerospace Plane Applications

Trajectory Optimization and Guidance Law Development for National Aerospace Plane Applications
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
Total Pages: 130
Release: 2018-07-23
Genre:
ISBN: 9781723464409

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The work completed to date is comprised of the following: a simple vehicle model representative of the aerospace plane concept in the hypersonic flight regime, fuel-optimal climb profiles for the unconstrained and dynamic pressure constrained cases generated using a reduced order dynamic model, an analytic switching condition for transition to rocket powered flight as orbital velocity is approached, simple feedback guidance laws for both the unconstrained and dynamic pressure constrained cases derived via singular perturbation theory and a nonlinear transformation technique, and numerical simulation results for ascent to orbit in the dynamic pressure constrained case. Calise, A. J. and Flandro, G. A. and Corban, J. E. Unspecified Center DYNAMIC MODELS; FEEDBACK CONTROL; FUEL CONSUMPTION; HYPERSONIC AIRCRAFT; OPTIMAL CONTROL; PERTURBATION THEORY; PRESSURE EFFECTS; SUPERSONIC COMBUSTION RAMJET ENGINES; WIND TUNNEL TESTS...

Advanced Guidance and Control of Flight Vehicle

Advanced Guidance and Control of Flight Vehicle
Author: Haizhao Liang
Publisher:
Total Pages: 0
Release: 2024-08-12
Genre: Mathematics
ISBN: 9783725818853

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The application of advanced guidance and control to missiles, hypersonic vehicles, and unmanned aerial vehicles has long represented a research hotspot in academia, and the development of more advanced and intelligent guidance and control technology for flight vehicles has become a focus of research in recent years. In this reprint, studies on the mathematical theory and application of flight vehicle guidance and control are presented. This includes trajectory optimization, online planning, advanced intermediate guidance theoretical methods, terminal guidance theoretical methods, intercept guidance and pursuit and escape guidance, and other topics.